STARLINK-31842, 59672
Orbit data source: Space-Track
STARLINK-31842, 59672 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 06 May 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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59672 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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-31842
1 59672U 24084U 25287.88805136 -.00000929 00000-0 -24264-4 0 9994
2 59672 43.0005 141.8330 0000958 277.5154 82.5588 15.27570451 82111Epoch: 2025-10-14T21:18Z
TLE epoch observation values (Epoch: 2025-10-14T21:18:47.637Z)
Latitude
-0.00007°
Longitude
158.46441°
Altitude
482.768 km
Speed
7.626 km/s
True Right ascension
09h 27m 19s
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
13:44:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.68 km
Perigee altitude
484.365 km
Semi-major axis
6,863.16 km
Eccentricity
0.0001
Inclination
43.0005°
RAAN
141.833°
Arg. of periapsis
277.5154°
True anomaly
82.56969°
Mean anomaly
82.5588°
Eccentric anomaly
82.56424°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
-0.000024264
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Other satellites on launch #84 in the year 2024 (2024-05-06 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-31842 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 19:34:38.281Z | 271.539° WNW | 2025-10-15 19:37:38.281Z | 323.935° NNW | 39.496° | 2025-10-15 19:41:38.281Z | 71.455° E |
| 6 mins | 2025-10-15 21:14:38.281Z | 293.066° NW | 2025-10-15 21:17:38.281Z | 42.403° NE | 38.892° | 2025-10-15 21:20:38.281Z | 88.834° E |
| 6 mins | 2025-10-15 22:53:38.281Z | 276.856° WNW | 2025-10-15 22:56:38.281Z | 177.106° S | 36.31° | 2025-10-15 22:59:38.281Z | 130.31° SE |
| 5 mins | 2025-10-16 17:29:38.281Z | 215.05° SW | 2025-10-16 17:31:38.281Z | 132.926° SE | 36.662° | 2025-10-16 17:34:38.281Z | 79.084° E |
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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