STARLINK-31676, 59900
Orbit data source: Space-Track
STARLINK-31676, 59900 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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59900 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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-31676
1 59900U 24100R 25354.03409745 .00000994 00000-0 45643-4 0 9999
2 59900 43.0009 215.3271 0001367 268.5493 91.5202 15.27581850 88867Epoch: 2025-12-20T00:49Z
TLE epoch observation values (Epoch: 2025-12-20T00:49:06.019Z)
Latitude
-0.00003°
Longitude
114.18529°
Altitude
482.844 km
Speed
7.626 km/s
True Right ascension
14h 21m 18s
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
21:33:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.927 km
Perigee altitude
484.05 km
Semi-major axis
6,863.126 km
Eccentricity
0.00014
Inclination
43.0009°
RAAN
215.3271°
Arg. of periapsis
268.5493°
True anomaly
91.53586°
Mean anomaly
91.5202°
Eccentric anomaly
91.52803°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.000045643
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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-31676 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 23:14:12.586Z | 283.679° WNW | 2025-12-20 23:17:12.586Z | 226.697° WSW | 41.357° | 2025-12-20 23:20:12.586Z | 124.981° SE |
| 5 mins | 2025-12-21 17:50:12.586Z | 213.264° SW | 2025-12-21 17:52:12.586Z | 167.746° S | 32.002° | 2025-12-21 17:55:12.586Z | 87.015° E |
| 5 mins | 2025-12-21 19:29:12.586Z | 270.307° WNW | 2025-12-21 19:31:12.586Z | 322.652° NNW | 41.654° | 2025-12-21 19:34:12.586Z | 68.057° E |
| 6 mins | 2025-12-21 21:08:12.586Z | 293.059° NW | 2025-12-21 21:10:12.586Z | 335.682° NNW | 37.539° | 2025-12-21 21:14:12.586Z | 84.408° 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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