TECHEDSAT 13, 51095 (Decayed)
Orbit data source: Space-Track
TECHEDSAT 13, 51095 was an American payload satellite in LEO that was launched on Thu, 13 Jan 2022 UTC via an LAUNCHERONE launch vehicle from the Pegasus Launch, Western Range Air Space (WRAS). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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51095 intel report (Beta)
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TECHEDSAT 13 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 4 months ago |
| Origin | |
| Manufacturer | ARC |
| Mission | Decayed Civil Technology |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 4 kg wet, 4 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Truss + 1 Sail, 0.8 m |
| Radar Cross Section | 0.035 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 4 months ago
0 TECHEDSAT 13
1 51095U 22003B 24194.23040869 .04907095 10302-4 89464-3 0 9997
2 51095 44.9616 175.9616 0003365 130.6448 229.4767 16.31437883140196Epoch: 2024-07-12T05:31Z
Definitive object data (Epoch: 2024-07-12T05:31:47.31Z)
| Latitude | -0.00003° |
| Longitude | 162.40477° |
| Altitude | 190.108 km |
| Speed | 7.793 km/s |
| True Right ascension | 11h 43m 50s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee | 192.577 km |
| Perigee | 188.156 km |
| Semi-major axis | 6,568.503 km |
| Eccentricity | 0.0003365 |
| Inclination | 44.9616° |
| RAAN | 175.9616° |
| Arg. of periapsis | 130.6448° |
| True anomaly | 229.4474° |
| Mean anomaly | 229.4767° |
| Eccentric anomaly | 229.46205° |
| Mean motion | 4.07703 °/min |
| BSTAR | 0.00089464 |
| Period | 88.3 mins |
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Other satellites on launch #3 in the year 2022 (2022-01-13 UTC)
TECHEDSAT 13 Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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