STARLINK-31995, 59958
Orbit data source: Space-Track
STARLINK-31995, 59958 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 05 Jun 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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59958 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-31995
1 59958U 24107P 26089.37132910 -.00000837 00000-0 -16155-4 0 9993
2 59958 53.1594 329.4138 0000873 97.3859 262.7241 15.30189985101762Epoch: 2026-03-30T08:54Z
TLE epoch observation values (Epoch: 2026-03-30T08:54:42.834Z)
Latitude
-0.00001°
Longitude
7.97149°
Altitude
476.22 km
Speed
7.629 km/s
True Right ascension
21h 57m 39s
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
02:47:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.1 km
Perigee altitude
474.903 km
Semi-major axis
6,853.638 km
Eccentricity
0.00009
Inclination
53.1594°
RAAN
329.4138°
Arg. of periapsis
97.3859°
True anomaly
262.71418°
Mean anomaly
262.7241°
Eccentric anomaly
262.71914°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
-0.000016155
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Other satellites on launch #107 in the year 2024 (2024-06-05 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-31995 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-31 01:04:52.963Z | 326.965° NNW | 2026-03-31 01:06:52.963Z | 18.979° NNE | 36.412° | 2026-03-31 01:09:52.963Z | 107.356° ESE |
| 5 mins | 2026-03-31 18:00:52.963Z | 196.816° SSW | 2026-03-31 18:02:52.963Z | 123.203° SE | 36.146° | 2026-03-31 18:05:52.963Z | 61.844° ENE |
| 4 mins | 2026-03-31 19:38:52.963Z | 289.073° WNW | 2026-03-31 19:40:52.963Z | 336.267° NNW | 23.121° | 2026-03-31 19:42:52.963Z | 19.559° NNE |
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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