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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31920
1 59907U 24100Y 25353.90231573 .00000301 00000-0 20454-4 0 9998
2 59907 43.0010 183.5513 0001167 272.4049 87.6669 15.27573015 89318Epoch: 2025-12-19T21:39Z
TLE epoch observation values (Epoch: 2025-12-19T21:39:20.079Z)
Latitude
-0°
Longitude
129.98083°
Altitude
482.813 km
Speed
7.626 km/s
True Right ascension
12h 14m 12s
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
19:33:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.816 km
Perigee altitude
484.214 km
Semi-major axis
6,863.152 km
Eccentricity
0.00012
Inclination
43.001°
RAAN
183.5513°
Arg. of periapsis
272.4049°
True anomaly
87.68026°
Mean anomaly
87.6669°
Eccentric anomaly
87.67358°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
0.000020454
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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 | 2025-12-20 21:40:10.301Z | 276.697° WNW | 2025-12-20 21:43:10.301Z | 218.055° SW | 31.877° | 2025-12-20 21:46:10.301Z | 144.149° SSE |
| 6 mins | 2025-12-21 16:16:10.301Z | 234.421° WSW | 2025-12-21 16:18:10.301Z | 192.341° SSW | 41.02° | 2025-12-21 16:22:10.301Z | 75.05° E |
| 6 mins | 2025-12-21 17:55:10.301Z | 281.548° WNW | 2025-12-21 17:57:10.301Z | 327.009° NNW | 37.877° | 2025-12-21 18:01:10.301Z | 72.654° E |
| 6 mins | 2025-12-21 19:34:10.301Z | 292.543° NW | 2025-12-21 19:37:10.301Z | 49.597° ENE | 40.817° | 2025-12-21 19:40:10.301Z | 94.278° ESE |
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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