STARLINK-31975, 59886
Orbit data source: Space-Track
STARLINK-31975, 59886 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 28 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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59886 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31975
1 59886U 24100B 25260.06992469 -.00001236 00000-0 -35389-4 0 9999
2 59886 43.0029 25.9407 0000792 287.2395 72.8370 15.27584008 74601Epoch: 2025-09-17T01:40Z
TLE epoch observation values (Epoch: 2025-09-17T01:40:41.493Z)
Latitude
-0°
Longitude
4.51665°
Altitude
482.653 km
Speed
7.626 km/s
True Right ascension
01h 43m 45s
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
17:34:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.525 km
Perigee altitude
484.438 km
Semi-major axis
6,863.119 km
Eccentricity
0.00008
Inclination
43.0029°
RAAN
25.9407°
Arg. of periapsis
287.2395°
True anomaly
72.84567°
Mean anomaly
72.837°
Eccentric anomaly
72.84134°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
-0.000035389
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Other satellites on launch #100 in the year 2024 (2024-05-28 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-31975 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 | 2025-09-18 10:49:11.420Z | 190.055° SSW | 2025-09-18 10:51:11.420Z | 154.141° SSE | 19.549° | 2025-09-18 10:54:11.420Z | 97.289° ESE |
| 5 mins | 2025-09-18 12:28:11.420Z | 248.176° W | 2025-09-18 12:30:11.420Z | 161.697° S | 44.936° | 2025-09-18 12:33:11.420Z | 72.487° E |
| 5 mins | 2025-09-18 14:07:11.420Z | 289.842° WNW | 2025-09-18 14:09:11.420Z | 350.015° N | 37.956° | 2025-09-18 14:12:11.420Z | 72.29° E |
| 6 mins | 2025-09-18 15:46:11.420Z | 291.187° WNW | 2025-09-18 15:48:11.420Z | 322.257° NNW | 43.457° | 2025-09-18 15:52:11.420Z | 103.448° ESE |
| 5 mins | 2025-09-18 17:25:11.420Z | 259.821° W | 2025-09-18 17:27:11.420Z | 213.313° SW | 25.245° | 2025-09-18 17:30:11.420Z | 154.324° SSE |
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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