STARLINK-31870, 59787
Orbit data source: Space-Track
STARLINK-31870, 59787 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 18 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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59787 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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-31870
1 59787U 24093F 26289.58965635 -.00001325 00000-0 -38615-4 0 9998
2 59787 43.0021 40.9874 0001752 262.2562 97.8091 15.27597801136481Epoch: 2026-10-16T14:09Z
TLE epoch observation values (Epoch: 2026-10-16T14:09:06.308Z)
Latitude
-0.00001°
Longitude
163.60261°
Altitude
482.935 km
Speed
7.626 km/s
True Right ascension
02h 43m 56s
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
14:39:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.143 km
Perigee altitude
483.738 km
Semi-major axis
6,863.078 km
Eccentricity
0.00018
Inclination
43.0021°
RAAN
40.9874°
Arg. of periapsis
262.2562°
True anomaly
97.82899°
Mean anomaly
97.8091°
Eccentric anomaly
97.81904°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
-0.000038615
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Other satellites on launch #93 in the year 2024 (2024-05-18 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-31870 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 | 2026-10-17 10:45:48.811Z | 212.525° SW | 2026-10-17 10:48:48.811Z | 131.339° SE | 36.362° | 2026-10-17 10:51:48.811Z | 81.967° E |
| 6 mins | 2026-10-17 12:24:48.811Z | 268.206° W | 2026-10-17 12:26:48.811Z | 309.034° NW | 60.897° | 2026-10-17 12:30:48.811Z | 70.274° E |
| 6 mins | 2026-10-17 14:03:48.811Z | 292.25° WNW | 2026-10-17 14:06:48.811Z | 31.3° NE | 49.964° | 2026-10-17 14:09:48.811Z | 82.332° E |
| 6 mins | 2026-10-17 15:42:48.811Z | 283.728° WNW | 2026-10-17 15:45:48.811Z | 161.845° S | 64.584° | 2026-10-17 15:48:48.811Z | 119.782° 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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