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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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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-31980
1 59962U 24107T 26089.38504724 -.00001532 00000-0 -39617-4 0 9996
2 59962 53.1618 329.4998 0001129 81.7876 278.3253 15.30187320102969Epoch: 2026-03-30T09:14Z
TLE epoch observation values (Epoch: 2026-03-30T09:14:28.081Z)
Latitude
-0.00001°
Longitude
3.10544°
Altitude
476.041 km
Speed
7.629 km/s
True Right ascension
21h 57m 59s
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
02:51:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.283 km
Perigee altitude
474.735 km
Semi-major axis
6,853.646 km
Eccentricity
0.00011
Inclination
53.1618°
RAAN
329.4998°
Arg. of periapsis
81.7876°
True anomaly
278.3125°
Mean anomaly
278.3253°
Eccentric anomaly
278.3189°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.000039617
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-31 01:25:55.895Z | 318.351° NNW | 2026-03-31 01:27:55.895Z | 73.37° E | 43.36° | 2026-03-31 01:30:55.895Z | 124.019° SE |
| 5 mins | 2026-03-31 18:20:55.895Z | 221.267° SW | 2026-03-31 18:22:55.895Z | 181.518° SSW | 43.492° | 2026-03-31 18:25:55.895Z | 53.954° ENE |
| 4 mins | 2026-03-31 19:59:55.895Z | 304.367° NW | 2026-03-31 20:01:55.895Z | 347.667° N | 18.398° | 2026-03-31 20:03:55.895Z | 22.336° NNE |
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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