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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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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-31870
1 59787U 24093F 25323.79965605 .00005061 00000-0 19338-3 0 9995
2 59787 43.0037 109.1117 0001728 264.4394 95.6261 15.27571206 85890Epoch: 2025-11-19T19:11Z
TLE epoch observation values (Epoch: 2025-11-19T19:11:30.282Z)
Latitude
-0°
Longitude
122.16932°
Altitude
482.968 km
Speed
7.626 km/s
True Right ascension
07h 16m 26s
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
22:28:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.206 km
Perigee altitude
483.834 km
Semi-major axis
6,863.157 km
Eccentricity
0.00017
Inclination
43.0037°
RAAN
109.1117°
Arg. of periapsis
264.4394°
True anomaly
95.64581°
Mean anomaly
95.6261°
Eccentric anomaly
95.63595°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
0.00019338
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-20 12:38:32.782Z | 199.497° SSW | 2025-11-20 12:41:32.782Z | 139.564° SSE | 22.736° | 2025-11-20 12:43:32.782Z | 99.204° ESE |
| 6 mins | 2025-11-20 14:17:32.782Z | 254.431° W | 2025-11-20 14:19:32.782Z | 265.652° W | 42.852° | 2025-11-20 14:23:32.782Z | 71.453° E |
| 6 mins | 2025-11-20 15:56:32.782Z | 288.205° WNW | 2025-11-20 15:59:32.782Z | 25.73° NE | 36.774° | 2025-11-20 16:02:32.782Z | 76.8° E |
| 6 mins | 2025-11-20 17:35:32.782Z | 288.76° WNW | 2025-11-20 17:38:32.782Z | 95.966° ESE | 44.172° | 2025-11-20 17:41:32.782Z | 107.594° ESE |
| 4 mins | 2025-11-20 19:15:32.782Z | 246.923° WSW | 2025-11-20 19:16:32.782Z | 224.479° SW | 21.688° | 2025-11-20 19:19:32.782Z | 163.551° S |
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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