STARLINK-31966, 59944
Orbit data source: Space-Track
STARLINK-31966, 59944 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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59944 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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-31966
1 59944U 24106Y 25289.66029272 .00000991 00000-0 45515-4 0 9997
2 59944 43.0019 66.0665 0001543 264.7212 95.3463 15.27587949 78547Epoch: 2025-10-16T15:50Z
TLE epoch observation values (Epoch: 2025-10-16T15:50:49.291Z)
Latitude
-0.00004°
Longitude
162.94425°
Altitude
482.9 km
Speed
7.626 km/s
True Right ascension
04h 24m 15s
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
03:26:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.029 km
Perigee altitude
483.911 km
Semi-major axis
6,863.107 km
Eccentricity
0.00015
Inclination
43.0019°
RAAN
66.0665°
Arg. of periapsis
264.7212°
True anomaly
95.3639°
Mean anomaly
95.3463°
Eccentric anomaly
95.3551°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.000045515
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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-31966 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 12:27:20.474Z | 216.481° SW | 2025-10-17 12:30:20.474Z | 144.742° SSE | 32.073° | 2025-10-17 12:33:20.474Z | 83.655° E |
| 5 mins | 2025-10-17 14:07:20.474Z | 273.295° WNW | 2025-10-17 14:09:20.474Z | 17.652° NNE | 41.612° | 2025-10-17 14:12:20.474Z | 69.814° E |
| 5 mins | 2025-10-17 15:46:20.474Z | 297.502° NW | 2025-10-17 15:48:20.474Z | 10.883° NNE | 38.967° | 2025-10-17 15:51:20.474Z | 81.992° E |
| 5 mins | 2025-10-17 17:25:20.474Z | 279.268° WNW | 2025-10-17 17:27:20.474Z | 199.481° SSW | 42.546° | 2025-10-17 17:30:20.474Z | 122.287° SE |
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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