STARLINK-31970, 59928
Orbit data source: Space-Track
STARLINK-31970, 59928 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 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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59928 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-31970
1 59928U 24106G 26085.89555131 .00001532 00000-0 65162-4 0 9999
2 59928 42.9979 235.4007 0001448 265.1563 94.9124 15.27586434103201Epoch: 2026-03-26T21:29Z
TLE epoch observation values (Epoch: 2026-03-26T21:29:35.633Z)
Latitude
0.00004°
Longitude
88.66434°
Altitude
482.89 km
Speed
7.626 km/s
True Right ascension
15h 41m 36s
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
17:18:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.969 km
Perigee altitude
483.982 km
Semi-major axis
6,863.112 km
Eccentricity
0.00014
Inclination
42.9979°
RAAN
235.4007°
Arg. of periapsis
265.1563°
True anomaly
94.92893°
Mean anomaly
94.9124°
Eccentric anomaly
94.92067°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.000065162
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Other satellites on launch #106 in the year 2024 (2024-06-01 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-31970 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 | 2026-03-27 13:24:20.046Z | 220.195° SW | 2026-03-27 13:27:20.046Z | 132.348° SE | 34.365° | 2026-03-27 13:30:20.046Z | 80.251° E |
| 6 mins | 2026-03-27 15:03:20.046Z | 272.044° WNW | 2026-03-27 15:06:20.046Z | 28.604° NE | 39.353° | 2026-03-27 15:09:20.046Z | 70.523° E |
| 5 mins | 2026-03-27 16:43:20.046Z | 299.861° NW | 2026-03-27 16:45:20.046Z | 27.139° NE | 39.173° | 2026-03-27 16:48:20.046Z | 85.572° E |
| 5 mins | 2026-03-27 18:22:20.046Z | 273.204° WNW | 2026-03-27 18:24:20.046Z | 183.482° SSW | 39.767° | 2026-03-27 18:27:20.046Z | 126.663° SE |
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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