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DECAYED
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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.

Not visible in the next 10 days
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TECHEDSAT 13 details
Identifier
51095, 2022-003B
Orbit
Decayed
Last TLE update4 months ago
Origin
Flag of USARC/SJSU (US)
ManufacturerARC
MissionDecayed Civil Technology
Bus & MotorCUBESAT 3U, Unknown motor
Mass4 kg wet, 4 kg dry
Launch date (UTC)
2022-01-13 (3 years ago)
Launch vehicle
LAUNCHERONE
Launch site
Pegasus Launch, Western Range Air Space (WRAS)
Object type
Payload
Rocket body
Debris
Shape & HBRBox + 1 Truss + 1 Sail, 0.8 m
Radar Cross Section0.035 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 16.31437883140196
Epoch: 2024-07-12T05:31Z
Definitive object data (Epoch: 2024-07-12T05:31:47.31Z)
Latitude-0.00003°
Longitude162.40477°
Altitude190.108 km
Speed7.793 km/s
True Right ascension11h 43m 50s
True Declination0° 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
Apogee192.577 km
Perigee188.156 km
Semi-major axis6,568.503 km
Eccentricity0.0003365
Inclination44.9616°
RAAN175.9616°
Arg. of periapsis130.6448°
True anomaly229.4474°
Mean anomaly229.4767°
Eccentric anomaly229.46205°
Mean motion4.07703 °/min
BSTAR0.00089464
Period88.3 mins
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TECHEDSAT 13 Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
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