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Soyuz FG Rocket Body
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Space Command ID: 39171
Launched: May 28, 2013 Re-Entry Prediction: May 31, 2013 - 15:19 UTC +/-1 Minute Inclination: 51.6° Re-Entry Zone: Pacific Ocean |
Re-Entry Ground Track
Image: Orbitron
Molniya 1-92
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Space Command ID: 27707
Launched: April 2, 2003 Re-Entry Prediction: May 27, 2013 Inclination: 63.8° Re-Entry Zone: Unknown |
Origin: CIS
Military Communications Satellite |
Kosmos 1188
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Space Command ID: 11844
Launched: June 14, 1980 Re-Entry Prediction: May 24, 2013 - 4:29 UTC +/-60 Minutes Inclination: 62.1° Re-Entry Zone: Unknown |
Origin: CIS
Oko Missile Early Warning Satellite |
Re-Entry Orbit
Image: Orbitron
F-1
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Space Command ID: 38855
Released from ISS: October 4, 2012 Re-Entry Prediction: May 9, 2013 - 19:58 UTC +/-26 Minutes Inclination: 51.6° Re-Entry Zone: Unknown |
F-1 was another one-unit CubeSat that was developed at FPT University and was designed to evaluate an advanced 3-axis magnetometer (SDTM). The 1-Kilogram vehicle included a low-resolution camera, body-mounted solar panels, micro-controllers, temperature sensors and VHF and UHF antennas.
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Tech-Ed-Sat
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Space Command ID: 38854
Released from ISS: October 4, 2012 Re-Entry Prediction: May 5, 2013 - 4:45 UTC +/-3 Hours Inclination: 51.6° Re-Entry Zone: Unknown Origin: USA |
TechEdSat was a one-unit CubeSat developed at the San Jose State University and performed several technical demonstrations. The vehicle evaluated Space Plug-and-play Avionics (SPA) designed in Sweden and performed a communications experiment utilizing the Iridium and Orbcomm satellite phone network. It had a mass of 1.19 Kilograms and featured a StenSat amateur beacon with 12 cm antenna for communications. Four rod magnets stabilized the satellite so that the Orcomm Antenna faced the sky while the beacon antenna looked down.
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Blok 2BL Rocket Body
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Space Command ID: 20539
Launched: March 27, 1990 Re-Entry Prediction: May 5, 2013 - 1:41 UTC +/-1 Minute Inclination: 60.8° Re-Entry Zone: Tasman/Fiji Sea |
Origin: CIS
Launched the Kosmos 2063 Spacecraft |
Re-Entry Ground Track
Image: Orbitron
Objects Orbited by Antares A-ONE
>>>Mission Site for Payload Information
Launched: April 21, 2013
Initial Orbit: 237 x 258 Kilometers
Inclination: 51.6°
Origin: USA/Orbital Sciences
Initial Orbit: 237 x 258 Kilometers
Inclination: 51.6°
Origin: USA/Orbital Sciences
Cygnus Mass Simulator
Space Command ID: 39142
Mass: 3,800kg Dimensions: 5.06 by 2.90m (Cylindrical) Re-Entry Prediction: May 10, 2013 - 00:58 UTC +/-7 Minutes Re-Entry Zone: Pacific Ocean, South America |
3 Phonesats
Space Command IDs: 39144, 39145, 39146
Type: 1-Unit Cubesats Mass: ~1kg Dimensions: 10x10x10cm Re-Entry Predictions: Alexander: April 27, 2013 - 9:37 UTC +/- 39 Minutes Graham: April 26, 2013 - 19:33 UTC +/- 4 Hours Bell: April 27, 2013 - 12:19 UTC +/-22 Minutes |
Dove-1
Space Command ID: 39143
Type: 3-Unit Cubesat Mass: 5.5kg Dimensions: 10x10x30cm Re-Entry Prediction: April 26, 2013 - 22:31 UTC +/-50 Minutes |
Castor 30A R/B
Space Command ID: 39147
Re-Entry Prediction: May 1, 2013 - 23:51 +/-7 Minutes Re-Entry Zone: Pacific Ocean |
Castor 30A Re-Entry Ground Track
Image: Orbitron
Cygnus Mass Simulator - Re-Entry Orbit
Image: Orbitron
