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 spacecraft
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 STARLINK-31968
1 59927U 24106F 25256.67341193 -.00000491 00000-0 -83304-5 0 9998
2 59927 42.9988 251.9441 0001018 264.5704 95.5031 15.27577119 73501Epoch: 2025-09-13T16:09Z
TLE epoch observation values (Epoch: 2025-09-13T16:09:42.79Z)
Latitude
-0.00006°
Longitude
16.61234°
Altitude
482.9 km
Speed
7.626 km/s
True Right ascension
16h 47m 46s
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
02:42:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.702 km
Perigee altitude
484.304 km
Semi-major axis
6,863.14 km
Eccentricity
0.0001
Inclination
42.9988°
RAAN
251.9441°
Arg. of periapsis
264.5704°
True anomaly
95.51471°
Mean anomaly
95.5031°
Eccentric anomaly
95.50891°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
-0.0000083304
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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 | 2025-09-15 02:54:10.039Z | 220.413° SW | 2025-09-15 02:57:10.039Z | 138.243° SSE | 34.49° | 2025-09-15 03:00:10.039Z | 81.052° E |
| 6 mins | 2025-09-15 04:33:10.039Z | 271.061° WNW | 2025-09-15 04:36:10.039Z | 21.674° NNE | 40.252° | 2025-09-15 04:39:10.039Z | 70.154° E |
| 5 mins | 2025-09-15 06:13:10.039Z | 298.586° NW | 2025-09-15 06:15:10.039Z | 18.684° NNE | 39.452° | 2025-09-15 06:18:10.039Z | 84.782° E |
| 5 mins | 2025-09-15 07:52:10.039Z | 274.895° WNW | 2025-09-15 07:54:10.039Z | 191.976° SSW | 40.454° | 2025-09-15 07:57:10.039Z | 126.484° 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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