STARLINK-31915, 59796 (Decayed)
Orbit data source: Space-Track
STARLINK-31915, 59796 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 18 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.
Focus sentinelFocus sentinel
59796 intel report (Beta)
Loading greatness...
STARLINK-31915 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 5 months 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 5 months ago
0 STARLINK-31915
1 59796U 24093Q 24155.76002328 .26324036 92744-5 35200-2 0 9998
2 59796 42.9880 275.4664 0006477 337.3134 139.2662 16.34370322 3868Epoch: 2024-06-03T18:14Z
Definitive object data (Epoch: 2024-06-03T18:14:26.011Z)
| Latitude | 37.70356° |
| Longitude | -126.3726° |
| Altitude | 185.964 km |
| Speed | 7.799 km/s |
| True Right ascension | 02h 39m 42s |
| True Declination | 37° 31' 22" |
| 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 | 187.107 km |
| Perigee | 178.608 km |
| Semi-major axis | 6,560.995 km |
| Eccentricity | 0.0006477 |
| Inclination | 42.988° |
| RAAN | 275.4664° |
| Arg. of periapsis | 337.3134° |
| True anomaly | 139.3146° |
| Mean anomaly | 139.2662° |
| Eccentric anomaly | 139.2904° |
| Mean motion | 4.08403 °/min |
| BSTAR | 0.00352 |
| Period | 88.15 mins |
Loading maneuver chart data...
Other satellites on launch #93 in the year 2024 (2024-05-18 UTC)
STARLINK-31915 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. |
|---|