STARLINK-31060, 58782 (Decayed)
Orbit data source: Space-Track
STARLINK-31060, 58782 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 14 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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58782 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Decayed 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: 6 months ago
TLE from 6 months ago
0 STARLINK-31060
1 58782U 24011T 25340.74354149 .14332580 12048-4 34338-2 0 9997
2 58782 53.1283 293.8650 0003974 88.7288 271.4210 16.28765963108189Epoch: 2025-12-06T17:50Z
TLE epoch observation values (Epoch: 2025-12-06T17:50:41.984Z)
Latitude
-0.00004°
Longitude
-49.57686°
Altitude
196.729 km
Speed
7.79 km/s
True Right ascension
19h 35m 27s
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
21:31:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
198.743 km
Perigee altitude
193.518 km
Semi-major axis
6,574.268 km
Eccentricity
0.0004
Inclination
53.1283°
RAAN
293.865°
Arg. of periapsis
88.7288°
True anomaly
271.37547°
Mean anomaly
271.421°
Eccentric anomaly
271.39824°
Mean motion
4.07167 °/min
Orbital period
88.42 mins
BSTAR
0.0034338
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Other satellites on launch #11 in the year 2024 (2024-01-14 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-31060 Visibility
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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. |
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| This satellite is decayed. |
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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