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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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: 19 hours ago
TLE from 19 hours ago
0 STARLINK-31968
1 59927U 24106F 26035.39281567 -.00001143 00000-0 -31967-4 0 9993
2 59927 43.0026 160.3015 0002837 309.4483 50.6118 15.27585992 95486Epoch: 2026-02-04T09:25Z
TLE epoch observation values (Epoch: 2026-02-04T09:25:39.273Z)
Latitude
0°
Longitude
-115.67218°
Altitude
481.572 km
Speed
7.627 km/s
True Right ascension
10h 41m 12s
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
06:18:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.923 km
Perigee altitude
483.029 km
Semi-major axis
6,863.113 km
Eccentricity
0.00028
Inclination
43.0026°
RAAN
160.3015°
Arg. of periapsis
309.4483°
True anomaly
50.63693°
Mean anomaly
50.6118°
Eccentric anomaly
50.62437°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
-0.000031967
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-05 10:42:59.000Z | 195.575° SSW | 2026-02-05 10:45:59.000Z | 140.932° SSE | 20.132° | 2026-02-05 10:47:59.000Z | 102.325° ESE |
| 6 mins | 2026-02-05 12:21:59.000Z | 249.242° W | 2026-02-05 12:23:59.000Z | 244.279° WSW | 42.742° | 2026-02-05 12:27:59.000Z | 72.234° E |
| 6 mins | 2026-02-05 14:00:59.000Z | 286.412° WNW | 2026-02-05 14:03:59.000Z | 24.569° NE | 36.795° | 2026-02-05 14:06:59.000Z | 75.177° E |
| 5 mins | 2026-02-05 15:40:59.000Z | 292.589° NW | 2026-02-05 15:42:59.000Z | 67.416° ENE | 43.865° | 2026-02-05 15:45:59.000Z | 103.462° ESE |
| 4 mins | 2026-02-05 17:19:59.000Z | 250.439° W | 2026-02-05 17:20:59.000Z | 226.685° WSW | 24.231° | 2026-02-05 17:23:59.000Z | 159.414° S |
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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