2007 April 7 - 17:31 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG 019. -
Soyuz TMA-10 Nation: Russia. Program: ISS. Payload: Soyuz TMA s/n 220 / ISS-14S. Mass: 7,200 kg (15,800 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TMA. Manufacturer: RKK Energia. Agency: Roskosmos. Perigee: 330 km (200 mi). Apogee: 341 km (211 mi). Inclination: 51.60 deg. Period: 91.20 min. COSPAR: 2007-008A. USAF Sat Cat: 31100. Duration: 196.71 days. Crew: Yurchikhin, Kotov, Simonyi. Flight: ISS EO-15, ISS EP-12. Carried the Expedition 15 crew and space tourist Charles Simonyi to the International Space Station. Soyuz TMA-10 docked at the Zarya port of the International Space Station at 19:10 GMT on 9 April. It undocked from Zarya at 19:20 GMT on Sep 27 September and docked at the Zvezda port at 19:47 GMT to clear Zarya for Soyuz TMA-10. The EO-15 crew and EP-13 space tourist Shukor (brought to the station by Soyuz TMA-11) boarded Soyuz TM-10 and undocked from the Zvezda port at 07:14 GMT on 21 October. The re-entry burn began at 09:47 and was normal. But afterwards, due to failure of an explosive bolt, the Soyuz service module remained connected to the re-entry capsule. The Soyuz tumbled, then began re-entry with the forward hatch taking the re-entry heating, until the connecting strut burned through. The Soyuz the righted itself with the heat shield taking the heating, but defaulted to an 8.6 G ballistic re-entry, landing 340 km short of the aim point at 10:36 GMT. Improved procedures after the ballistic re-entry of Soyuz TMA-1 meant a helicopter recovery crew reached the capsule only 20 minutes after thumpdown. However the true nature of the failure was concealed from the world until the same thing happened on Soyuz TMA-11.
References: 2.
2007 April 9 - 22:54 GMT - Launch Site: Baikonur. Launch Complex: LC200/39. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-M/Briz-M. LV Configuration: Proton-M/Briz-M 535-16. -
Anik F3 Nation: Canada. Payload: Eurostar 3000S. Mass: 4,634 kg (10,216 lb). Class: Communications. Spacecraft: Eurostar 3000. Manufacturer: Astrium. Agency: Telesat Canada. Perigee: 35,781 km (22,233 mi). Apogee: 35,795 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.20 min. COSPAR: 2007-009A. USAF Sat Cat: 31102. Communications satellite with C, Ku and Ka band transponders. References: 2.
2007 April 11 - 03:27 GMT - Launch Site: Taiyuan. Launch Complex: -. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-29 (96). -
Haiyang 1B Nation: China. Class: Surveillance. Type: Ocean. Spacecraft: HY-1. Manufacturer: AS-DFH-Sat Ltd. Agency: CASC. Perigee: 782 km (485 mi). Apogee: 815 km (506 mi). Inclination: 98.60 deg. Period: 100.80 min. COSPAR: 2007-010A. USAF Sat Cat: 31113. Oceanographic satellite equipped with a 10-band ocean color scanner, a 4-band CCD imager with 250-meter resolution, and an infrared water profile radiometer. References: 2.
2007 April 12 - 20:11 GMT - Launch Site: Xichang. Launch Complex: -. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-13 (97). -
Beidou 5 Nation: China. Payload: Beidou M1. Mass: 2,200 kg (4,800 lb). Class: Navigation. Spacecraft: Beidou. Manufacturer: CAST. Agency: CASC. Perigee: 21,519 km (13,371 mi). Apogee: 21,544 km (13,386 mi). Inclination: 55.30 deg. Period: 773.40 min. COSPAR: 2007-011A. USAF Sat Cat: 31115. The fifth Beidou satellite, but the first in the 12-hour, 55 deg inclination MEO portion of the constellation. All previous launches had been to populate the geostationary portion of the system. References: 2.
2007 April 17 - 06:46 GMT - Launch Site: Baikonur. Launch Complex: LC109. Launch Pad: LC109/95. Launch Vehicle: R-36M. Model: Dnepr. LV Configuration: Dnepr 806. -
MisrSat 1 Nation: Egypt. Payload: Egyptsat 1 / MS-1TK. Mass: 100 kg (220 lb). Class: Surveillance. Spacecraft: MS-1. Manufacturer: NPO Yuzhnoye. Agency: NARSSS. Perigee: 657 km (408 mi). Apogee: 667 km (414 mi). Inclination: 98.10 deg. Period: 98.00 min. COSPAR: 2007-012A. USAF Sat Cat: 31117. MisrSat/Egyptsat carried an imaging payload for Egypt's National Authority for Remote Sensing and Space Sciences. References: 2.
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Saudisat 3 Nation: Saudi Arabia. Mass: 35 kg (77 lb). Class: Surveillance. Manufacturer: RSRI. Agency: RSRI. Perigee: 656 km (407 mi). Apogee: 679 km (421 mi). Inclination: 98.10 deg. Period: 98.10 min. COSPAR: 2007-012B. USAF Sat Cat: 31118. Saudisat 3 carried a suveillance instrument, backed by data collection and relay avionics, to work in concert with the five smaller SaudiComSats launched at the same time. References: 2.
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SaudiComsat-7 Nation: Saudi Arabia. Mass: 12 kg (26 lb). Class: Communications. Manufacturer: RSRI. Agency: RSRI. Perigee: 651 km (404 mi). Apogee: 740 km (450 mi). Inclination: 98.10 deg. Period: 98.70 min. COSPAR: 2007-012C. USAF Sat Cat: 31119. References: 2.
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SaudiComsat-6 Nation: Saudi Arabia. Mass: 12 kg (26 lb). Class: Communications. Manufacturer: RSRI. Agency: RSRI. Perigee: 649 km (403 mi). Apogee: 762 km (473 mi). Inclination: 98.10 deg. Period: 98.90 min. COSPAR: 2007-012E. USAF Sat Cat: 31121. References: 2.
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Aerocube 2 Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Aerospace. Agency: AeroSpace. Perigee: 648 km (402 mi). Apogee: 771 km (479 mi). Inclination: 98.10 deg. Period: 99.00 min. COSPAR: 2007-012F. USAF Sat Cat: 31122. AeroSpace Corporation cubesat. References: 2.
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SaudiComsat-5 Nation: Saudi Arabia. Mass: 12 kg (26 lb). Class: Communications. Manufacturer: RSRI. Agency: RSRI. Perigee: 652 km (405 mi). Apogee: 729 km (452 mi). Inclination: 98.10 deg. Period: 98.60 min. COSPAR: 2007-012H. USAF Sat Cat: 31124. References: 2.
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SaudiComsat-3 Nation: Saudi Arabia. Mass: 12 kg (26 lb). Class: Communications. Manufacturer: RSRI. Agency: RSRI. Perigee: 653 km (405 mi). Apogee: 718 km (446 mi). Inclination: 98.10 deg. Period: 98.50 min. COSPAR: 2007-012J. USAF Sat Cat: 31125. References: 2.
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MAST Nation: USA. Mass: 3.00 kg (6.60 lb). Class: Technology. Type: Tether. Spacecraft: Cubesat. Manufacturer: Stanford SSDL. Agency: Tethers Unltd. Perigee: 647 km (402 mi). Apogee: 783 km (486 mi). Inclination: 98.10 deg. Period: 99.10 min. COSPAR: 2007-012K. USAF Sat Cat: 31126. Multi Application Survivable Tether experiment, built by Tethers Unlimited Inc and Stanford University. MAST consisted of the TED (Tether Deployer) satellite, with a 1 km deployable multi-strand Hoytether; RALPH, a small end mass satellite; and between them, GADGET, an inspector satellite which could move along the tether. Before deployment the MAST package fit into a 0.3 m x 0.1 m module.
References: 2.
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SaudiComsat-4 Nation: Saudi Arabia. Mass: 12 kg (26 lb). Class: Communications. Manufacturer: RSRI. Agency: RSRI. Perigee: 650 km (400 mi). Apogee: 751 km (466 mi). Inclination: 98.10 deg. Period: 98.80 min. COSPAR: 2007-012L. USAF Sat Cat: 31127. References: 2.
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CP 3 Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Cal Poly. Agency: Cal Poly. Perigee: 646 km (401 mi). Apogee: 793 km (492 mi). Inclination: 98.10 deg. Period: 99.20 min. COSPAR: 2007-012M. USAF Sat Cat: 31128. California Polytechnic University cubesat, the backup for CP2 lost in a Dnepr launch failure in 2006. References: 2.
- Libertad Nation: Colombia. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Un. S. Arboleda. Agency: Un. S. Arboleda. Perigee: 646 km (401 mi). Apogee: 793 km (492 mi). Inclination: 98.10 deg. Period: 99.20 min. COSPAR: 2007-012N. USAF Sat Cat: 31129. Picosat built and operated by the Universidad Sergio Arboleda, Bogota, Colombia. References: 2.
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CAPE 1 Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: University of Louisiana. Agency: University of Louisiana. Perigee: 646 km (401 mi). Apogee: 793 km (492 mi). Inclination: 98.10 deg. Period: 99.20 min. COSPAR: 2007-012P. USAF Sat Cat: 31130. Cajun Advanced Picosatellite Experiment by the University of Louisiana at Lafayette. References: 2.
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CP 4 Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Cal Poly. Agency: Cal Poly. Perigee: 648 km (402 mi). Apogee: 771 km (479 mi). Inclination: 98.10 deg. Period: 99.00 min. COSPAR: 2007-012Q. USAF Sat Cat: 31132. California Polytechnic University cubesat. References: 2.
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CSTB 1 Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Boeing. Agency: Boeing. Perigee: 648 km (402 mi). Apogee: 771 km (479 mi). Inclination: 98.10 deg. Period: 99.00 min. COSPAR: 2007-012R. USAF Sat Cat: 31133. CubeSat TestBed for Boeing IDS/Advanced Systems, Huntington Beach, California. References: 2.
2007 April 21 - 12:31 GMT -
2007 April 23 - 10:00 GMT - Launch Site: Sriharikota. Launch Complex: SLP. Launch Pad: -. Launch Vehicle: PSLV. Model: PSLV. LV Configuration: PSLV-CA PSLV-C8. -
AGILE Nation: Italy. Mass: 352 kg (776 lb). Class: Astronomy. Spacecraft: AGILE. Manufacturer: Carlo Gavazzi. Agency: ASI. Perigee: 523 km (324 mi). Apogee: 553 km (343 mi). Inclination: 2.50 deg. Period: 95.40 min. COSPAR: 2007-013A. USAF Sat Cat: 31135. The PSLV-C8 launch vehicle flew for the first time in a light configuration with
no strap-on motors and a Dual Launch Adapter. The Italian gamma-ray observatory satellite (Astrorivelatore Gamma ad Imagini Leggero) carried the GRID 0.3-200 MeV wide-field gamma ray camera and the Super-AGILE 15-45 keV detector hard X-ray detector.
References: 2.
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AAM Nation: India. Mass: 185 kg (407 lb). Class: Technology. Manufacturer: ISRO. Agency: ISRO. Perigee: 531 km (329 mi). Apogee: 549 km (341 mi). Inclination: 2.50 deg. Period: 95.50 min. COSPAR: 2007-013B. USAF Sat Cat: 31136. The Dual Launch Adapter housed the secondary payload, an Advanced Avionics Module for future use on Indian launch vehicles. The AAM remained attached to the PSLV fourth stage. References: 2.
2007 April 24 - 06:48 GMT - Launch Site: Wallops Island. Launch Complex: LA0B. Launch Pad: -. Launch Vehicle: Minotaur. Model: Minotaur 1. LV Configuration: Minotaur 1 7. -
NFIRE Nation: USA. Payload: SA-200B. Mass: 494 kg (1,089 lb). Class: Technology. Spacecraft: SA-200. Manufacturer: Spectrum Astro. Agency: USAFRL. Perigee: 489 km (303 mi). Apogee: 497 km (308 mi). Inclination: 48.20 deg. Period: 94.50 min. COSPAR: 2007-014A. USAF Sat Cat: 31140. Near Field Infrared Experiment conducted by the US Missile Defense Agency. Its Track Sensor Payload included visible and short, medium and long wave infrared
sensors to observe missiles launched from the ground, and obtain basic data to distinguish between the missile and its hot rocket exhaust plume for application to anti-ballistic missile systems. Secondary payloads included Tesat, a German laser communications terminal, and its hydrazine propulsion system. This was used to maneuver the satellite from its initial 255 km x 465 km x 48.2 deg orbit to 489 km x 497 km by 18 May. The orbit was changed to 243 km x 487 km on 9 August and by 23 August was 219 km x 450 km. The satellite had a dry mass of 380 kg dry, was 2.7 m long and 1.3 m in diameter.The first major sensor test occurred when Minotaur II rocket TLV-7, was
fired at 08:30 GMT on 23 August from Vandenberg in NFIRE Mission 2a. The Minotaur II was aimed to pass within 4 and 20 km of the NFIRE satellite while its third stage motor burning, to allow NFIRE to get a close look at the rocket and its exhaust. The Missile Defense Agency reported that the experiment was successful.
References: 2.
2007 April 25 - 20:26 GMT - Launch Site: Point Arguello WADZ. Launch Complex: -. Launch Pad: 36.0 N x 123.0 W. Launch Vehicle: Pegasus. Model: Pegasus XL. LV Configuration: Pegasus XL F38. -
AIM Nation: USA. Mass: 150 kg (330 lb). Spacecraft: RS-300. Manufacturer: OSC, Ball. Agency: NASA, Hampton U. Perigee: 584 km (362 mi). Apogee: 602 km (374 mi). Inclination: 97.80 deg. Period: 96.50 min. COSPAR: 2007-015A. USAF Sat Cat: 31304. NASA Small Explorer mission, for Aeronomy of Ice in the Mesosphere. AIM carried three scientific instruments to study polar mesospheric clouds: a solar occultation camera, an ultraviolet imager, and a cosmic dust experiment. References: 2.
2007 May 4 - 22:29 GMT - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5ECA. LV Configuration: Ariane 5ECA V176 (536). -
Astra 1L Nation: Luxembourg. Program: Astra. Payload: A2100AX. Mass: 4,497 kg (9,914 lb). Class: Communications. Spacecraft: AS 2100. Manufacturer: Lockheed Martin, Sunnyvale. Agency: SES Astra. Perigee: 35,784 km (22,235 mi). Apogee: 35,788 km (22,237 mi). Inclination: 0.10 deg. Period: 1,436.00 min. COSPAR: 2007-016A. USAF Sat Cat: 31306. Astra 1L provided direct-to-home broadcast services to Europe from its location at 19.2º East. It also strengthened the SES in-orbit backup system, extended fleet coverage from the Canary Islands eastwards up to the Russian border, and allowed Astra 2C to be moved from 19.2º East to 28.2º to fulfill high capacity demand from the U.K. and Ireland. Astra 1L was equipped with 29 Ku + 2 Ka active transponders, which would be reduced to 27 active transponders after its first five years of operation.
References: 2.
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Galaxy 17 Nation: USA. Program: Galaxy. Payload: SB-3000B3. Mass: 4,100 kg (9,000 lb). Class: Communications. Spacecraft: Spacebus 3000. Manufacturer: Thales Alenia Space. Agency: Intelsat. Perigee: 35,785 km (22,235 mi). Apogee: 35,789 km (22,238 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2007-016B. USAF Sat Cat: 31307. C/Ku-band satellite for cable television relay in the United States. References: 2.
2007 May 12 - 03:25 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz-U. LV Configuration: Soyuz-U Ts15000-104 / ISS-25P. -
Progress M-60 Nation: Russia. Program: ISS. Payload: Progress M s/n 360. Mass: 7,280 kg (16,040 lb). Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energia. Agency: Roskosmos. Perigee: 330 km (200 mi). Apogee: 341 km (211 mi). Inclination: 51.60 deg. Period: 91.20 min. COSPAR: 2007-017A. USAF Sat Cat: 31393. Duration: 136.65 days. Flight: ISS EO-15, ISS EO-14-1. Space station resupply spacecraft which docked with the Zvezda port of the International Space Station at 05:10 GMT on 15 May. It undocked on 19 September was conducted plasma depletion experiments before being deorbited over the Pacific at 19:01 GMT on 25 September..
References: 2.
2007 May 13 - 16:01 GMT - Launch Site: Xichang. Launch Complex: -. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B (98). -
Nigcomsat 1 Nation: Nigeria. Mass: 5,150 kg (11,350 lb). Class: Communications. Spacecraft: DFH-4. Agency: Nigerian Communications Satellite Ltd. Perigee: 35,782 km (22,233 mi). Apogee: 35,789 km (22,238 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2007-018A. USAF Sat Cat: 31395. Second DFH-4 communications satellite; China's first commercial payload sale, and Nigeria's first commercial communications satellite. Positioned at 42.5 deg E. Payload consisted of 4 C-band, 14 Ku-band, 8 Ka-band, and 2 L-band transponders. The antenna subsystem consisted of seven antennas.
References: 2.
2007 May 15 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-37. -
Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
2007 May 15 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-37. -
FCET-37 Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
2007 May 25 - 07:12 GMT - Launch Site: Jiuquan. Launch Complex: -. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-2D. LV Configuration: Chang Zheng 2D CZ2D-8 (99). -
Yaogan 2 Nation: China. Mass: 2,700 kg (5,900 lb). Class: Surveillance. Type: Military Radarsat. Spacecraft: Yaogan. Manufacturer: CAST. Agency: CNSA. Perigee: 631 km (392 mi). Apogee: 655 km (406 mi). Inclination: 97.80 deg. Period: 97.60 min. COSPAR: 2007-019A. USAF Sat Cat: 31490. Second Chinese synthetic aperture radar military surveillance satellite. References: 2.
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Zheda Pixing 1 Nation: China. Mass: 2.00 kg (4.40 lb). Class: Technology. Manufacturer: SIMIT. Agency: Zhejiang University. COSPAR: 2007-019x. Experimental microelectronics research picosatellite. References: 2.
2007 May 25 - 14:15 GMT - Launch Site: Kodiak. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: STARS. LV Configuration: STARS M-9. FAILURE: Failure. -
GMD FTG-03 Target Nation: USA. Agency: USA SMDC. Apogee: 40 km (24 mi). References: 2.
2007 May 29 - 10:20 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Topol. Model: Topol M. LV Configuration: Topol-M RS-24 Yars. -
ICBM Test Nation: Russia. Agency: RVSN RF. Apogee: 1,000 km (600 mi). First test of a new Russian heavyweight, mobile, solid propellant ICBM. The multiple test warheads were said to have impacted on target 5,500 km down range in the Kura Test Range in the Kamchatka Peninsula. Although development must have been underway for some time, the launch was touted as a reply to American plans to install ABM system elements in the Czech Republic and Poland.
References: 2.
2007 May 29 - 20:31 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG/Fregat Ts15000-021. -
Globalstar A Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 914 km (567 mi). Apogee: 932 km (579 mi). Inclination: 52.00 deg. Period: 103.50 min. COSPAR: 2007-020A. USAF Sat Cat: 31571. First replenishment launch of the resurgent Globalstar MEO communications satellite constellation after a five-year hiatus. References: 2.
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Globalstar B Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 913 km (567 mi). Apogee: 931 km (578 mi). Inclination: 52.00 deg. Period: 103.50 min. COSPAR: 2007-020C. USAF Sat Cat: 31573. References: 2.
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Globalstar C Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 926 km (575 mi). Apogee: 932 km (579 mi). Inclination: 52.00 deg. Period: 103.60 min. COSPAR: 2007-020D. USAF Sat Cat: 31574. References: 2.
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Globalstar D Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 919 km (571 mi). Apogee: 938 km (582 mi). Inclination: 52.00 deg. Period: 103.60 min. COSPAR: 2007-020F. USAF Sat Cat: 31576. References: 2.
2007 May 31 - 16:08 GMT - Launch Site: Xichang. Launch Complex: -. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-14 (100). -
Sinosat 3 Nation: China. Mass: 2,200 kg (4,800 lb). Class: Communications. Spacecraft: DFH-3. Manufacturer: CAST. Agency: SinoSatCom. Perigee: 35,779 km (22,231 mi). Apogee: 35,793 km (22,240 mi). Inclination: 0.30 deg. Period: 1,436.10 min. COSPAR: 2007-021A. USAF Sat Cat: 31577. Chinese C-band domestic communications satellite, launched as part of a campaign to prepare for the 2008 Olympic Games, and to compensate for failure of the first DFH-4 satellite. References: 2.
2007 June 7 - 18:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz-U. -
Cosmos 2427 Nation: Russia. Mass: 6,700 kg (14,700 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4K1. Manufacturer: TsSKB-Progress. Agency: VKS. Perigee: 167 km (103 mi). Apogee: 339 km (210 mi). Inclination: 67.10 deg. Period: 89.80 min. COSPAR: 2007-022A. USAF Sat Cat: 31595. Duration: 76.13 days. Recoverable capsule military optical reconnaisance satellite. Orbit was raised on 11 June to 182 km x 354 km; decayed until 19 June, when it was lowered to 175 km x 325 km. On 28 June the orbit was raised to 183 km x 348 km; on 5 July to 169 km x 375 km. Landed at 21:00 GMT on 22 August after a 76-day mission.
References: 2.
2007 June 8 - 02:34 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7420-10C. LV Configuration: Delta 7420-10C D324. -
Cosmo-SkyMed 1 Nation: Italy. Mass: 1,700 kg (3,700 lb). Class: Surveillance. Type: Radarsat. Spacecraft: Cosmo-SkyMed. Manufacturer: Thales Alenia Space. Agency: ASI. Perigee: 622 km (386 mi). Apogee: 626 km (388 mi). Inclination: 97.90 deg. Period: 97.20 min. COSPAR: 2007-023A. USAF Sat Cat: 31598. The first of four Constellation of Small Satellites for Mediterranean basin Observation, Synthetic Aperture Radar satellites for primarily Italian military surveillance, but with products made available to civilian users as well. References: 2.
2007 June 8 - 23:38 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-117. -
STS-117 Nation: USA. Program: ISS. Payload: Atlantis F28 / S3, S4. Mass: 122,685 kg (270,474 lb). Class: Manned. Type: Spaceplane. Spacecraft: Atlantis. Manufacturer: Boeing. Agency: NASA. Perigee: 330 km (200 mi). Apogee: 341 km (211 mi). Inclination: 51.60 deg. Period: 91.20 min. COSPAR: 2007-024A. USAF Sat Cat: 31600. Duration: 13.84 days. Crew: Sturckow, Archambault, Forrester, Swanson, Olivas, Reilly, Anderson Clayton. Flight: ISS EO-15, ISS EO-14-1, STS-117, ISS EO-15-1. The shuttle delivered the S3 and S4 truss segments to the starboard side of the International Space Station. The crew made three spacewalks to install these truss segments, conduct other station reconfiguration and installation work, deploy the solar arrays and prepare them for operation. A fourth spacewalk was added to repair loose re-entry insulation on the shuttle and get-ahead installation work on the outside of the station. The shuttle delivered NASA long-term ISS crew member Clayton Anderson to the station; and returned Suni Williams to earth. At the conclusion of this mission the station finally achieved its full-power, dual-boom configuration first conceived for Space Station Freedom in the 1980's.
References: 2.
2007 June 10 - 23:40 GMT - Launch Site: Palmachim. Launch Complex: -. Launch Pad: -. Launch Vehicle: Shavit. Model: Shavit 1. LV Configuration: Shaviyt 1 7. -
Ofeq-7 Nation: Israel. Program: Offeq. Mass: 300 kg (660 lb). Class: Surveillance. Type: Military. Spacecraft: Ofeq 5. Manufacturer: IAI-MBT. Agency: Tsahal. Perigee: 340 km (210 mi). Apogee: 576 km (357 mi). Inclination: 141.80 deg. Period: 93.80 min. COSPAR: 2007-025A. USAF Sat Cat: 31601. Israeli optical reconnaisance satellite, evidently using an improved version of the Shavit booster and probably heavier and more capable than its predecessors. References: 2.
2007 June 15 - 02:14 GMT - Launch Site: Baikonur. Launch Complex: LC109. Launch Pad: LC109/95. Launch Vehicle: R-36M. Model: Dnepr. -
TerraSAR-X Nation: Germany. Mass: 1,346 kg (2,967 lb). Class: Surveillance. Type: Radarsat. Spacecraft: TerraSAR-X. Manufacturer: EADS Astrium. Agency: DLR/EADS Astrium. Perigee: 499 km (310 mi). Apogee: 512 km (318 mi). Inclination: 97.50 deg. COSPAR: 2007-026A. USAF Sat Cat: 31701. Scientific/commercial surveillance satellite. equipped with an X-band synthetic aperture radar with 1 meter resolution References: 2.
2007 June 15 - 15:11 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: SLC41. Launch Vehicle: Atlas V. Model: Atlas V 401. LV Configuration: Atlas V 401 AV-009. -
USA 194 Nation: USA. Class: SIGINT. Spacecraft: NOSS-3. Manufacturer: Lockheed Martin. Agency: NRO. Perigee: 776 km (482 mi). Apogee: 1,246 km (774 mi). Inclination: 63.00 deg. COSPAR: 2007-027A. USAF Sat Cat: 31701. Classified National Reconnaissance Office mission. There appeared to be problem in the second burn of the Centaur upper stage. Amateur observors believed that two satellites were to be have been deployed in 1150 km altitude, 63 deg inclination, but that only a 776 km x 1246 km was achieved. However it was believed that the payloads could reach the final intended orbits using on-board propulsion
References: 2.
2007 June 21 - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: MSBS. Model: MSBS M51. LV Configuration: MSBS M51 2. -
M51 SLBM test Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi). References: 2.
2007 June 22 - 19:50 GMT -
2007 June 28 - Launch Site: White Sea Launch Area. Launch Complex: -. Launch Pad: 65.5 N x 38.0 E. Launch Vehicle: Bulava. -
Bulava SLBM test Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). The warhead impacted on target in the Kamchatka Peninsula. This was the first successful launch after two consecutive failures. References: 2.
2007 June 28 - 15:02 GMT - Launch Site: Dombarovskiy. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-36M. Model: Dnepr. -
Genesis 2 Nation: USA. Mass: 1,360 kg (2,990 lb). Class: Manned. Type: Space Station Module. Spacecraft: Genesis Pathfinder. Manufacturer: Bigelow. Agency: Bigelow. Perigee: 556 km (345 mi). Apogee: 561 km (348 mi). Inclination: 64.50 deg. Period: 95.80 min. COSPAR: 2007-028A. USAF Sat Cat: 31789. One third scale version of the privately-financed Nautilus inflatable human space habitat module. The spacecraft's 22 interior and exterior cameras provided images of items and pictures carried for paying participants in Bigelow's Fly your Stuff program.
References: 2.
2007 June 29 - 10:00 GMT - Launch Site: Baikonur. Launch Complex: LC45/1. Launch Pad: -. Launch Vehicle: Zenit. Model: Zenit-2SLB. LV Configuration: Zenit-2M 1-2005. -
Cosmos 2428 Nation: Russia. Mass: 3,200 kg (7,000 lb). Class: Sigint. Spacecraft: Tselina-2. Manufacturer: Yuzhnoye. Agency: VKS. Perigee: 846 km (525 mi). Apogee: 857 km (532 mi). Inclination: 71.00 deg. Period: 102.00 min. COSPAR: 2007-029A. USAF Sat Cat: 31792. Signals intelligence satellite. First launch in three years, and first with the improved version of the Zenit-2 launch vehicle using components developed for the Zenit-3SL. References: 2.
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