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: 1 day ago
TLE from 1 day ago
0 STARLINK-31968
1 59927U 24106F 26080.77098420 .00000219 00000-0 17472-4 0 9995
2 59927 42.9994 264.0232 0001461 200.2971 159.7822 15.27589600102429Epoch: 2026-03-21T18:30Z
TLE epoch observation values (Epoch: 2026-03-21T18:30:13.034Z)
Latitude
-0.00009°
Longitude
167.18188°
Altitude
483.736 km
Speed
7.625 km/s
True Right ascension
17h 36m 05s
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
04:19:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.968 km
Perigee altitude
483.963 km
Semi-major axis
6,863.103 km
Eccentricity
0.00015
Inclination
42.9994°
RAAN
264.0232°
Arg. of periapsis
200.2971°
True anomaly
159.78798°
Mean anomaly
159.7822°
Eccentric anomaly
159.78509°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.000017472
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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 | 2026-03-23 14:38:21.188Z | 204.819° SW | 2026-03-23 14:41:21.188Z | 139.569° SSE | 25.784° | 2026-03-23 14:44:21.188Z | 86.899° E |
| 6 mins | 2026-03-23 16:17:21.188Z | 259.633° W | 2026-03-23 16:19:21.188Z | 282.014° WNW | 41.881° | 2026-03-23 16:23:21.188Z | 70.822° E |
| 5 mins | 2026-03-23 17:57:21.188Z | 299.074° NW | 2026-03-23 17:59:21.188Z | 23.934° NE | 37.287° | 2026-03-23 18:02:21.188Z | 78.601° E |
| 5 mins | 2026-03-23 19:36:21.188Z | 285.774° WNW | 2026-03-23 19:38:21.188Z | 137.211° SSE | 44.255° | 2026-03-23 19:41:21.188Z | 112.384° ESE |
| 4 mins | 2026-03-23 21:15:21.188Z | 244.6° WSW | 2026-03-23 21:16:21.188Z | 224.03° SW | 18.899° | 2026-03-23 21:19:21.188Z | 168.372° 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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