STARLINK-31360, 58982 (Decayed)
Orbit data source: Space-Track
STARLINK-31360, 58982 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 15 Feb 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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58982 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: 1 year ago
TLE from 1 year ago
0 STARLINK-31360
1 58982U 24031T 25039.13840833 .15217798 11787-4 48453-2 0 9995
2 58982 53.1309 309.8583 0012345 215.0869 310.9607 16.25364394 56399Epoch: 2025-02-08T03:19Z
TLE epoch observation values (Epoch: 2025-02-08T03:19:18.479Z)
Latitude
11.19592°
Longitude
-66.94676°
Altitude
199.871 km
Speed
7.792 km/s
True Right ascension
08h 05m 28s
True Declination
11° 07' 30"
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
21:28:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
213.426 km
Perigee altitude
197.171 km
Semi-major axis
6,583.436 km
Eccentricity
0.00123
Inclination
53.1309°
RAAN
309.8583°
Arg. of periapsis
215.0869°
True anomaly
310.85376°
Mean anomaly
310.9607°
Eccentric anomaly
310.90724°
Mean motion
4.06316 °/min
Orbital period
88.6 mins
BSTAR
0.0048453
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Other satellites on launch #31 in the year 2024 (2024-02-15 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-31360 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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