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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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Partially 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-31920
1 59907U 24100Y 26306.33335647 .00259365 32544-4 82129-3 0 9995
2 59907 42.9791 121.5397 0027767 290.9087 277.3859 15.89820625 6032Epoch: 2026-11-02T08:00Z
TLE epoch observation values (Epoch: 2026-11-02T08:00:01.999Z)
Latitude
-18.80762°
Longitude
161.23011°
Altitude
304.484 km
Speed
7.727 km/s
True Right ascension
21h 31m 24s
True Declination
-18° 41' 45"
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
14:34:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
323.343 km
Perigee altitude
286.23 km
Semi-major axis
6,682.923 km
Eccentricity
0.00278
Inclination
42.9791°
RAAN
121.5397°
Arg. of periapsis
290.9087°
True anomaly
277.07021°
Mean anomaly
277.3859°
Eccentric anomaly
277.22807°
Mean motion
3.97277 °/min
Orbital period
90.62 mins
BSTAR
0.00082129
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-02 19:36:31.747Z | 292.783° NW | 2026-11-02 19:38:31.747Z | 55.443° ENE | 68.821° | 2026-11-02 19:40:31.747Z | 100.901° ESE |
| 4 mins | 2026-11-03 16:35:31.747Z | 279.429° WNW | 2026-11-03 16:36:31.747Z | 311.825° NW | 46.063° | 2026-11-03 16:39:31.747Z | 67.314° ENE |
| 4 mins | 2026-11-03 18:10:31.747Z | 302.495° NW | 2026-11-03 18:12:31.747Z | 37.918° NE | 37.591° | 2026-11-03 18:14:31.747Z | 79.168° E |
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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