STARLINK-31965, 59888
Orbit data source: Space-Track
STARLINK-31965, 59888 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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59888 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-31965
1 59888U 24100D 26126.41872007 .00021245 00000-0 77894-3 0 9993
2 59888 43.0028 159.5632 0002865 293.1041 66.9508 15.27594632109883Epoch: 2026-05-06T10:02Z
TLE epoch observation values (Epoch: 2026-05-06T10:02:57.414Z)
Latitude
-0.00004°
Longitude
144.54444°
Altitude
482.012 km
Speed
7.627 km/s
True Right ascension
10h 38m 15s
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
03:03:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.916 km
Perigee altitude
482.984 km
Semi-major axis
6,863.087 km
Eccentricity
0.00029
Inclination
43.0028°
RAAN
159.5632°
Arg. of periapsis
293.1041°
True anomaly
66.98101°
Mean anomaly
66.9508°
Eccentric anomaly
66.96591°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.00077894
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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-31965 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 | 2026-05-07 05:04:06.138Z | 205.684° SW | 2026-05-07 05:07:06.138Z | 149.016° SSE | 24.832° | 2026-05-07 05:10:06.138Z | 90.278° ESE |
| 5 mins | 2026-05-07 06:44:06.138Z | 259.692° W | 2026-05-07 06:46:06.138Z | 32.415° NE | 43.963° | 2026-05-07 06:49:06.138Z | 70.652° E |
| 5 mins | 2026-05-07 08:23:06.138Z | 294.979° NW | 2026-05-07 08:25:06.138Z | 5.294° NNE | 38.046° | 2026-05-07 08:28:06.138Z | 76.43° E |
| 5 mins | 2026-05-07 10:02:06.138Z | 287.435° WNW | 2026-05-07 10:04:06.138Z | 252.747° W | 44.916° | 2026-05-07 10:07:06.138Z | 110.617° ESE |
| 4 mins | 2026-05-07 11:41:06.138Z | 250.644° W | 2026-05-07 11:43:06.138Z | 207.353° SW | 20.073° | 2026-05-07 11:45:06.138Z | 170.229° 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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