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.
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51097 intel report (Beta)
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GEARRS-3 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 3 months ago |
| Origin | |
| Manufacturer | NearSpaceLaunch |
| Mission | Decayed Commercial Communications |
| 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, 0.3 m |
| Radar Cross Section | 0.035 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 16.45547106144304Epoch: 2024-08-07T17:04Z
Definitive object data (Epoch: 2024-08-07T17:04:52.096Z)
| Latitude | -0.00003° |
| Longitude | 170.7763° |
| Altitude | 148.876 km |
| Speed | 7.82 km/s |
| True Right ascension | 01h 34m 49s |
| True Declination | 0° 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
| Apogee | 158.206 km |
| Perigee | 147.382 km |
| Semi-major axis | 6,530.931 km |
| Eccentricity | 0.0008286 |
| Inclination | 44.9127° |
| RAAN | 23.7043° |
| Arg. of periapsis | 294.0535° |
| True anomaly | 66.03915° |
| Mean anomaly | 65.9524° |
| Eccentric anomaly | 65.99577° |
| Mean motion | 4.11226 °/min |
| BSTAR | 0.00032982 |
| Period | 87.54 mins |
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Other satellites on launch #3 in the year 2022 (2022-01-13 UTC)
GEARRS-3 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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