STARLINK-31976, 59887
Orbit data source: Space-Track
STARLINK-31976, 59887 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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59887 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-31976
1 59887U 24100C 26306.18997494 -.00000504 00000-0 -87835-5 0 9999
2 59887 43.0031 228.0605 0001266 264.6055 95.4652 15.27579595137430Epoch: 2026-11-02T04:33Z
TLE epoch observation values (Epoch: 2026-11-02T04:33:33.834Z)
Latitude
-0.00005°
Longitude
118.19892°
Altitude
482.909 km
Speed
7.626 km/s
True Right ascension
15h 12m 14s
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
12:20:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.864 km
Perigee altitude
484.126 km
Semi-major axis
6,863.132 km
Eccentricity
0.00013
Inclination
43.0031°
RAAN
228.0605°
Arg. of periapsis
264.6055°
True anomaly
95.47964°
Mean anomaly
95.4652°
Eccentric anomaly
95.47242°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
-0.0000087835
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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-31976 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 | 2026-11-02 22:00:43.411Z | 213.044° SW | 2026-11-02 22:03:43.411Z | 160.132° S | 31.973° | 2026-11-02 22:06:43.411Z | 90.095° ESE |
| 5 mins | 2026-11-02 23:40:43.411Z | 264.532° W | 2026-11-02 23:42:43.411Z | 328.432° NNW | 71.444° | 2026-11-02 23:45:43.411Z | 68.82° E |
| 6 mins | 2026-11-03 01:19:43.411Z | 293.304° NW | 2026-11-03 01:21:43.411Z | 343.569° N | 49.945° | 2026-11-03 01:25:43.411Z | 80.931° E |
| 6 mins | 2026-11-03 02:58:43.411Z | 285.754° WNW | 2026-11-03 03:00:43.411Z | 264.899° W | 67.594° | 2026-11-03 03:04:43.411Z | 114.52° 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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