STARLINK-31260, 58881
Orbit data source: Space-Track
STARLINK-31260, 58881 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 29 Jan 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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58881 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: 2 days ago
TLE from 2 days ago
0 STARLINK-31260
1 58881U 24020F 26171.36174117 .00002065 00000-0 72279-4 0 9999
2 58881 53.1598 204.6018 0001153 82.9151 277.1983 15.34383876133800Epoch: 2026-06-20T08:40Z
TLE epoch observation values (Epoch: 2026-06-20T08:40:54.437Z)
Latitude
0.00003°
Longitude
165.79754°
Altitude
463.554 km
Speed
7.636 km/s
True Right ascension
13h 38m 24s
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
21:34:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.797 km
Perigee altitude
462.219 km
Semi-major axis
6,841.145 km
Eccentricity
0.00012
Inclination
53.1598°
RAAN
204.6018°
Arg. of periapsis
82.9151°
True anomaly
277.18519°
Mean anomaly
277.1983°
Eccentric anomaly
277.19175°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
0.000072279
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Other satellites on launch #20 in the year 2024 (2024-01-29 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-31260 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 | 2026-06-22 11:12:06.609Z | 313.051° NW | 2026-06-22 11:15:06.609Z | 41.431° NE | 44.363° | 2026-06-22 11:18:06.609Z | 125.654° SE |
| 6 mins | 2026-06-23 04:05:06.609Z | 221.85° SW | 2026-06-23 04:08:06.609Z | 78.7° E | 41.759° | 2026-06-23 04:11:06.609Z | 53.056° ENE |
| 4 mins | 2026-06-23 05:44:06.609Z | 303.772° NW | 2026-06-23 05:46:06.609Z | 347.224° N | 18.048° | 2026-06-23 05:48:06.609Z | 22.221° NNE |
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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