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 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: 20 hours ago
TLE from 20 hours ago
0 STARLINK-31975
1 59886U 24100B 25310.74441108 .00002601 00000-0 10399-3 0 9997
2 59886 43.0042 99.7569 0001638 273.4959 86.5706 15.27583201 82357Epoch: 2025-11-06T17:51Z
TLE epoch observation values (Epoch: 2025-11-06T17:51:57.117Z)
Latitude
0.00003°
Longitude
145.57062°
Altitude
482.748 km
Speed
7.626 km/s
True Right ascension
06h 39m 01s
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
10:09:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.108 km
Perigee altitude
483.86 km
Semi-major axis
6,863.121 km
Eccentricity
0.00016
Inclination
43.0042°
RAAN
99.7569°
Arg. of periapsis
273.4959°
True anomaly
86.58934°
Mean anomaly
86.5706°
Eccentric anomaly
86.57997°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00010399
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-07 14:31:20.328Z | 254.633° W | 2025-11-07 14:34:20.328Z | 274.387° WNW | 43.439° | 2025-11-07 14:38:20.328Z | 71.359° E |
| 6 mins | 2025-11-07 16:11:20.328Z | 289.171° WNW | 2025-11-07 16:14:20.328Z | 30.244° NE | 36.305° | 2025-11-07 16:17:20.328Z | 77.57° E |
| 6 mins | 2025-11-07 17:50:20.328Z | 288.416° WNW | 2025-11-07 17:53:20.328Z | 105.367° ESE | 43.632° | 2025-11-07 17:56:20.328Z | 108.666° ESE |
| 4 mins | 2025-11-07 19:30:20.328Z | 244.591° WSW | 2025-11-07 19:31:20.328Z | 221.991° SW | 21.197° | 2025-11-07 19:34:20.328Z | 163.665° S |
| 5 mins | 2025-11-08 12:26:20.328Z | 189.511° SSW | 2025-11-08 12:28:20.328Z | 144.104° SSE | 23.058° | 2025-11-08 12:31:20.328Z | 90.301° ESE |
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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