STARLINK-31980, 59962
Orbit data source: Space-Track
STARLINK-31980, 59962 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 05 Jun 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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59962 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-31980
1 59962U 24107T 25364.51191512 -.00000586 00000-0 -76609-5 0 9994
2 59962 53.1604 26.9497 0001044 109.8153 250.2960 15.30188258 89209Epoch: 2025-12-30T12:17Z
TLE epoch observation values (Epoch: 2025-12-30T12:17:09.466Z)
Latitude
-0.00005°
Longitude
103.46609°
Altitude
476.391 km
Speed
7.629 km/s
True Right ascension
01h 47m 47s
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
00:39:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.222 km
Perigee altitude
474.791 km
Semi-major axis
6,853.643 km
Eccentricity
0.0001
Inclination
53.1604°
RAAN
26.9497°
Arg. of periapsis
109.8153°
True anomaly
250.28474°
Mean anomaly
250.296°
Eccentric anomaly
250.29037°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.0000076609
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Other satellites on launch #107 in the year 2024 (2024-06-05 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-31980 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 | 2025-12-31 04:07:57.135Z | 212.227° SW | 2025-12-31 04:10:57.135Z | 124.576° SE | 39.761° | 2025-12-31 04:13:57.135Z | 58.884° ENE |
| 5 mins | 2025-12-31 10:43:57.135Z | 331.212° NNW | 2025-12-31 10:45:57.135Z | 43.759° NE | 36.854° | 2025-12-31 10:48:57.135Z | 109.81° ESE |
| 4 mins | 2025-12-31 12:21:57.135Z | 262.492° W | 2025-12-31 12:23:57.135Z | 220.211° SW | 17.858° | 2025-12-31 12:25:57.135Z | 186.33° SSW |
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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