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DECAYED
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GEARRS-3, 51097 (Decayed)

Orbit data source: Space-Track

GEARRS-3, 51097 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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GEARRS-3 details
Identifier
51097, 2022-003D
Orbit
Decayed
Last TLE update3 months ago
Origin
Flag of USNSL/AFRL (US)
ManufacturerNearSpaceLaunch
MissionDecayed Commercial Communications
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, 0.3 m
Radar Cross Section0.035 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 months ago
0 GEARRS-3
1 51097U 22003D   24220.71171408  .13367639  10692-4  32982-3 0  9995
2 51097  44.9127  23.7043 0008286 294.0535  65.9524 16.45547106144304
Epoch: 2024-08-07T17:04Z
Definitive object data (Epoch: 2024-08-07T17:04:52.096Z)
Latitude-0.00003°
Longitude170.7763°
Altitude148.876 km
Speed7.82 km/s
True Right ascension01h 34m 49s
True Declination0° 00' 00"
Sunlit
Object was in full shadow 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
Apogee158.206 km
Perigee147.382 km
Semi-major axis6,530.931 km
Eccentricity0.0008286
Inclination44.9127°
RAAN23.7043°
Arg. of periapsis294.0535°
True anomaly66.03915°
Mean anomaly65.9524°
Eccentric anomaly65.99577°
Mean motion4.11226 °/min
BSTAR0.00032982
Period87.54 mins
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GEARRS-3 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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