STARLINK-31968, 59927
Orbit data source: Space-Track
STARLINK-31968, 59927 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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59927 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: 5 hours ago
TLE from 5 hours ago
0 STARLINK-31968
1 59927U 24106F 26127.98000949 .00000996 00000-0 45731-4 0 9990
2 59927 43.0010 357.4136 0001044 277.2462 82.8271 15.27576749109641Epoch: 2026-05-07T23:31Z
TLE epoch observation values (Epoch: 2026-05-07T23:31:12.819Z)
Latitude
-0.00004°
Longitude
138.79178°
Altitude
482.745 km
Speed
7.626 km/s
True Right ascension
23h 49m 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
12:18:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.72 km
Perigee altitude
484.287 km
Semi-major axis
6,863.141 km
Eccentricity
0.0001
Inclination
43.001°
RAAN
357.4136°
Arg. of periapsis
277.2462°
True anomaly
82.83897°
Mean anomaly
82.8271°
Eccentric anomaly
82.83303°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.000045731
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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-31968 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 | 2026-05-08 18:33:24.686Z | 218.351° SW | 2026-05-08 18:36:24.686Z | 153.993° SSE | 32.386° | 2026-05-08 18:39:24.686Z | 84.873° E |
| 5 mins | 2026-05-08 20:13:24.686Z | 271.926° WNW | 2026-05-08 20:15:24.686Z | 356.025° N | 42.259° | 2026-05-08 20:18:24.686Z | 69.184° E |
| 5 mins | 2026-05-08 21:52:24.686Z | 295.47° NW | 2026-05-08 21:54:24.686Z | 355.635° N | 38.895° | 2026-05-08 21:57:24.686Z | 81.135° E |
| 5 mins | 2026-05-08 23:31:24.686Z | 280.244° WNW | 2026-05-08 23:33:24.686Z | 223.331° SW | 42.084° | 2026-05-08 23:36:24.686Z | 123.332° 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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