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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-31838
1 60130U 24118T 25293.38555801 -.00001066 00000-0 -23888-4 0 9990
2 60130 53.1608 318.5249 0001203 104.1462 255.9672 15.30188146 74218Epoch: 2025-10-20T09:15Z
TLE epoch observation values (Epoch: 2025-10-20T09:15:12.212Z)
Latitude
-0.00004°
Longitude
150.63536°
Altitude
476.35 km
Speed
7.629 km/s
True Right ascension
21h 14m 05s
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
19:44:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.331 km
Perigee altitude
474.682 km
Semi-major axis
6,853.644 km
Eccentricity
0.00012
Inclination
53.1608°
RAAN
318.5249°
Arg. of periapsis
104.1462°
True anomaly
255.95383°
Mean anomaly
255.9672°
Eccentric anomaly
255.96051°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.000023888
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-21 04:14:07.746Z | 214.479° SW | 2025-10-21 04:17:07.746Z | 129.346° SE | 40.92° | 2025-10-21 04:20:07.746Z | 58.027° ENE |
| 4 mins | 2025-10-21 05:54:07.746Z | 308.195° NW | 2025-10-21 05:55:07.746Z | 332.079° NNW | 20.838° | 2025-10-21 05:58:07.746Z | 27.525° NE |
| 5 mins | 2025-10-21 10:50:07.746Z | 328.964° NNW | 2025-10-21 10:52:07.746Z | 39.754° NE | 37.933° | 2025-10-21 10:55:07.746Z | 111.074° ESE |
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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