STARLINK-31838, 60130
Orbit data source: Space-Track
STARLINK-31838, 60130 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 24 Jun 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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60130 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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31838
1 60130U 24118T 26306.43550096 .00020982 00000-0 68599-3 0 9996
2 60130 53.1598 0.4776 0001053 62.2340 297.8768 15.31700772132122Epoch: 2026-11-02T10:27Z
TLE epoch observation values (Epoch: 2026-11-02T10:27:07.282Z)
Latitude
-0.00005°
Longitude
161.98466°
Altitude
471.301 km
Speed
7.632 km/s
True Right ascension
00h 01m 54s
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
05:12:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.716 km
Perigee altitude
470.273 km
Semi-major axis
6,849.131 km
Eccentricity
0.00011
Inclination
53.1598°
RAAN
0.4776°
Arg. of periapsis
62.234°
True anomaly
297.86613°
Mean anomaly
297.8768°
Eccentric anomaly
297.87147°
Mean motion
3.82904 °/min
Orbital period
94.02 mins
BSTAR
0.00068599
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Other satellites on launch #118 in the year 2024 (2024-06-24 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-31838 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 11:58:32.968Z | 346.488° N | 2026-11-03 12:00:32.968Z | 32.37° NE | 23.508° | 2026-11-03 12:02:32.968Z | 73.221° E |
| 5 mins | 2026-11-03 13:36:32.968Z | 291.119° WNW | 2026-11-03 13:38:32.968Z | 209.795° SW | 53.114° | 2026-11-03 13:41:32.968Z | 148.034° SSE |
| 5 mins | 2026-11-04 06:30:32.968Z | 252.32° W | 2026-11-04 06:32:32.968Z | 309.789° NW | 53.392° | 2026-11-04 06:35:32.968Z | 38.997° NE |
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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