STARLINK-31958, 59924
Orbit data source: Space-Track
STARLINK-31958, 59924 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 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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59924 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: 1 day ago
TLE from 1 day ago
0 STARLINK-31958
1 59924U 24106C 25361.39223382 .00009363 00000-0 34867-3 0 9993
2 59924 43.0098 6.3061 0002588 272.2875 87.7681 15.27642894 89638Epoch: 2025-12-27T09:24Z
TLE epoch observation values (Epoch: 2025-12-27T09:24:49.002Z)
Latitude
0.00004°
Longitude
128.98274°
Altitude
482.569 km
Speed
7.626 km/s
True Right ascension
00h 25m 13s
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
18:03:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.58 km
Perigee altitude
483.028 km
Semi-major axis
6,862.941 km
Eccentricity
0.00026
Inclination
43.0098°
RAAN
6.3061°
Arg. of periapsis
272.2875°
True anomaly
87.79773°
Mean anomaly
87.7681°
Eccentric anomaly
87.78292°
Mean motion
3.81749 °/min
Orbital period
94.3 mins
BSTAR
0.00034867
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Other satellites on launch #106 in the year 2024 (2024-06-01 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-31958 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-29 02:23:33.303Z | 176.669° S | 2025-12-29 02:25:33.303Z | 142.592° SSE | 15.059° | 2025-12-29 02:27:33.303Z | 108.344° ESE |
| 6 mins | 2025-12-29 04:01:33.303Z | 237.504° WSW | 2025-12-29 04:04:33.303Z | 107.875° ESE | 40.668° | 2025-12-29 04:07:33.303Z | 74.723° E |
| 6 mins | 2025-12-29 05:40:33.303Z | 281.658° WNW | 2025-12-29 05:43:33.303Z | 23.982° NE | 37.325° | 2025-12-29 05:46:33.303Z | 72.46° E |
| 5 mins | 2025-12-29 07:20:33.303Z | 297.309° NW | 2025-12-29 07:22:33.303Z | 40.422° NE | 42.059° | 2025-12-29 07:25:33.303Z | 95.282° ESE |
| 5 mins | 2025-12-29 08:59:33.303Z | 258.887° W | 2025-12-29 09:01:33.303Z | 192.861° SSW | 30.638° | 2025-12-29 09:04:33.303Z | 141.245° SSE |
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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