STARLINK-31920, 59907
Orbit data source: Space-Track
STARLINK-31920, 59907 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 28 May 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft 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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59907 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 STARLINK-31920
1 59907U 24100Y 25323.36684830 .00000211 00000-0 17194-4 0 9990
2 59907 43.0072 356.0009 0002031 271.3523 88.7096 15.27582544 84643Epoch: 2025-11-19T08:48Z
TLE epoch observation values (Epoch: 2025-11-19T08:48:15.693Z)
Latitude
-0.00001°
Longitude
165.2959°
Altitude
482.787 km
Speed
7.626 km/s
True Right ascension
23h 44m 00s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.379 km
Perigee altitude
483.592 km
Semi-major axis
6,863.122 km
Eccentricity
0.0002
Inclination
43.0072°
RAAN
356.0009°
Arg. of periapsis
271.3523°
True anomaly
88.73287°
Mean anomaly
88.7096°
Eccentric anomaly
88.72123°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.000017194
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Other satellites on launch #100 in the year 2024 (2024-05-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-31920 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-20 05:23:55.482Z | 214.365° SW | 2025-11-20 05:26:55.482Z | 160.172° S | 28.707° | 2025-11-20 05:29:55.482Z | 89.267° E |
| 5 mins | 2025-11-20 07:03:55.482Z | 265.793° W | 2025-11-20 07:05:55.482Z | 331.856° NNW | 43.302° | 2025-11-20 07:08:55.482Z | 69.054° E |
| 5 mins | 2025-11-20 08:42:55.482Z | 293.313° NW | 2025-11-20 08:44:55.482Z | 344.337° N | 37.809° | 2025-11-20 08:47:55.482Z | 77.446° E |
| 6 mins | 2025-11-20 10:21:55.482Z | 284.241° WNW | 2025-11-20 10:23:55.482Z | 254.26° W | 42.569° | 2025-11-20 10:27:55.482Z | 116.418° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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