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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31870
1 59787U 24093F 25308.95692929 -.00000396 00000-0 -48709-5 0 9996
2 59787 43.0000 192.9369 0001458 265.7322 94.3364 15.27579730 83623Epoch: 2025-11-04T22:57Z
TLE epoch observation values (Epoch: 2025-11-04T22:57:58.690Z)
Latitude
0.00004°
Longitude
164.00589°
Altitude
482.901 km
Speed
7.626 km/s
True Right ascension
12h 51m 44s
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
18:04:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.996 km
Perigee altitude
483.994 km
Semi-major axis
6,863.132 km
Eccentricity
0.00015
Inclination
43°
RAAN
192.9369°
Arg. of periapsis
265.7322°
True anomaly
94.35306°
Mean anomaly
94.3364°
Eccentric anomaly
94.34473°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
-0.0000048709
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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 | 2025-11-05 22:52:21.010Z | 290.015° WNW | 2025-11-05 22:55:21.010Z | 14.675° NNE | 38.6° | 2025-11-05 22:58:21.010Z | 81.167° E |
| 5 mins | 2025-11-06 00:32:21.010Z | 280.629° WNW | 2025-11-06 00:34:21.010Z | 190.929° SSW | 43.253° | 2025-11-06 00:37:21.010Z | 119.893° SE |
| 5 mins | 2025-11-06 19:07:21.010Z | 205.233° SW | 2025-11-06 19:09:21.010Z | 153.473° SSE | 30.162° | 2025-11-06 19:12:21.010Z | 86.677° E |
| 5 mins | 2025-11-06 20:46:21.010Z | 268.652° W | 2025-11-06 20:48:21.010Z | 358.382° N | 42.957° | 2025-11-06 20:51:21.010Z | 69.413° E |
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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