STARLINK-31957, 59926
Orbit data source: Space-Track
STARLINK-31957, 59926 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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59926 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-31957
1 59926U 24106E 26081.22099467 .00007338 00000-0 27589-3 0 9995
2 59926 43.0030 261.3809 0001430 269.6039 90.4649 15.27581680102496Epoch: 2026-03-22T05:18Z
TLE epoch observation values (Epoch: 2026-03-22T05:18:13.939Z)
Latitude
-0.00001°
Longitude
2.09234°
Altitude
482.828 km
Speed
7.626 km/s
True Right ascension
17h 25m 31s
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
00:50:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.97 km
Perigee altitude
484.007 km
Semi-major axis
6,863.126 km
Eccentricity
0.00014
Inclination
43.003°
RAAN
261.3809°
Arg. of periapsis
269.6039°
True anomaly
90.48129°
Mean anomaly
90.4649°
Eccentric anomaly
90.47309°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
0.00027589
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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-31957 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 | 2026-03-22 19:50:47.707Z | 288.302° WNW | 2026-03-22 19:53:47.707Z | 293.316° NW | 42.596° | 2026-03-22 19:57:47.707Z | 108.084° ESE |
| 4 mins | 2026-03-22 21:31:47.707Z | 241.365° WSW | 2026-03-22 21:32:47.707Z | 217.403° SW | 21.769° | 2026-03-22 21:35:47.707Z | 161.173° S |
| 4 mins | 2026-03-23 14:27:47.707Z | 185.945° SSW | 2026-03-23 14:29:47.707Z | 139.121° SSE | 22.467° | 2026-03-23 14:31:47.707Z | 99.207° ESE |
| 6 mins | 2026-03-23 16:05:47.707Z | 254.011° W | 2026-03-23 16:07:47.707Z | 264.481° W | 43.065° | 2026-03-23 16:11:47.707Z | 71.527° E |
| 6 mins | 2026-03-23 17:44:47.707Z | 288.233° WNW | 2026-03-23 17:47:47.707Z | 26.979° NE | 36.614° | 2026-03-23 17:50:47.707Z | 76.761° E |
| 6 mins | 2026-03-23 19:23:47.707Z | 288.901° WNW | 2026-03-23 19:26:47.707Z | 94.45° ESE | 43.996° | 2026-03-23 19:29:47.707Z | 107.243° ESE |
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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