STARLINK-31102, 58715
Orbit data source: Space-Track
STARLINK-31102, 58715 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 03 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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58715 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-31102
1 58715U 24002L 26171.43304081 -.00007853 00000-0 -22193-3 0 9999
2 58715 53.1611 112.1450 0001800 82.5234 277.5973 15.34338948137753Epoch: 2026-06-20T10:23Z
TLE epoch observation values (Epoch: 2026-06-20T10:23:34.725Z)
Latitude
-0.00005°
Longitude
47.60254°
Altitude
463.624 km
Speed
7.636 km/s
True Right ascension
07h 28m 34s
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
21:38:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.373 km
Perigee altitude
461.91 km
Semi-major axis
6,841.278 km
Eccentricity
0.00018
Inclination
53.1611°
RAAN
112.145°
Arg. of periapsis
82.5234°
True anomaly
277.57685°
Mean anomaly
277.5973°
Eccentric anomaly
277.58708°
Mean motion
3.83564 °/min
Orbital period
93.86 mins
BSTAR
-0.00022193
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Other satellites on launch #2 in the year 2024 (2024-01-03 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-31102 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 21:58:21.100Z | 219.971° SW | 2026-06-22 22:01:21.100Z | 142.486° SSE | 43.159° | 2026-06-22 22:04:21.100Z | 55.346° ENE |
| 5 mins | 2026-06-23 04:33:21.100Z | 325.489° NNW | 2026-06-23 04:35:21.100Z | 39.16° NE | 39.822° | 2026-06-23 04:38:21.100Z | 114.73° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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