STARLINK-31894, 59665 (Decayed)
Orbit data source: Space-Track
STARLINK-31894, 59665 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 06 May 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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59665 intel report (Beta)
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STARLINK-31894 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 1 month ago |
| Origin | |
| Manufacturer | SpaceX/Seattle |
| Mission | Decayed spacecraft |
| Bus & Motor | STARLINK V2M, Unknown motor |
| Mass | 800 kg wet, ~750 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 STARLINK-31894
1 59665U 24084M 24263.09663046 .09667759 90625-5 20651-2 0 9992
2 59665 42.9799 180.3365 0006562 252.7832 240.2526 16.29697157 22409Epoch: 2024-09-19T02:19Z
Definitive object data (Epoch: 2024-09-19T02:19:08.871Z)
| Latitude | 30.04023° |
| Longitude | -71.03636° |
| Altitude | 196.03 km |
| Speed | 7.792 km/s |
| True Right ascension | 21h 28m 57s |
| True Declination | 29° 52' 43" |
| 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 | 199.701 km |
| Perigee | 191.074 km |
| Semi-major axis | 6,573.525 km |
| Eccentricity | 0.0006562 |
| Inclination | 42.9799° |
| RAAN | 180.3365° |
| Arg. of periapsis | 252.7832° |
| True anomaly | 240.18734° |
| Mean anomaly | 240.2526° |
| Eccentric anomaly | 240.21997° |
| Mean motion | 4.07236 °/min |
| BSTAR | 0.0020651 |
| Period | 88.4 mins |
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Other satellites on launch #84 in the year 2024 (2024-05-06 UTC)
STARLINK-31894 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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