STARLINK-31320, 58886
Orbit data source: Space-Track
STARLINK-31320, 58886 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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58886 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-31320
1 58886U 24020L 26171.38059292 .00002713 00000-0 91443-4 0 9996
2 58886 53.1605 204.0106 0001265 86.2404 273.8743 15.34385853133813Epoch: 2026-06-20T09:08Z
TLE epoch observation values (Epoch: 2026-06-20T09:08:03.228Z)
Latitude
-0.00003°
Longitude
158.40109°
Altitude
463.588 km
Speed
7.636 km/s
True Right ascension
13h 36m 02s
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
21:33:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.867 km
Perigee altitude
462.137 km
Semi-major axis
6,841.139 km
Eccentricity
0.00013
Inclination
53.1605°
RAAN
204.0106°
Arg. of periapsis
86.2404°
True anomaly
273.85984°
Mean anomaly
273.8743°
Eccentric anomaly
273.86707°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
0.000091443
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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-31320 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 11:40:08.966Z | 300.143° NW | 2026-06-22 11:43:08.966Z | 240.688° WSW | 37.749° | 2026-06-22 11:46:08.966Z | 150.812° SSE |
| 5 mins | 2026-06-23 04:34:08.966Z | 254.033° W | 2026-06-23 04:36:08.966Z | 336.258° NNW | 39.268° | 2026-06-23 04:39:08.966Z | 41.443° NE |
| 4 mins | 2026-06-23 09:30:08.966Z | 346.607° N | 2026-06-23 09:32:08.966Z | 29.257° NE | 19.198° | 2026-06-23 09:34:08.966Z | 68.221° E |
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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