STARLINK-36251, 68093
Orbit data source: Space-Track
STARLINK-36251, 68093 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 04 Mar 2026 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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68093 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 STARLINK-36251
1 68093U 26042AA 26170.96461574 .00018529 00000-0 55865-3 0 9995
2 68093 53.1594 62.2674 0001272 95.4935 264.6213 15.34372351 17971Epoch: 2026-06-19T23:09Z
TLE epoch observation values (Epoch: 2026-06-19T23:09:02.799Z)
Latitude
-0.00002°
Longitude
166.81969°
Altitude
463.768 km
Speed
7.636 km/s
True Right ascension
04h 09m 04s
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
07:19:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.913 km
Perigee altitude
462.172 km
Semi-major axis
6,841.179 km
Eccentricity
0.00013
Inclination
53.1594°
RAAN
62.2674°
Arg. of periapsis
95.4935°
True anomaly
264.60679°
Mean anomaly
264.6213°
Eccentric anomaly
264.61404°
Mean motion
3.83572 °/min
Orbital period
93.85 mins
BSTAR
0.00055865
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Other satellites on launch #42 in the year 2026 (2026-03-04 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-36251 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 21:18:46.243Z | 303.404° NW | 2026-06-20 21:20:46.243Z | 339.427° N | 15.523° | 2026-06-20 21:22:46.243Z | 15.735° NNE |
| 5 mins | 2026-06-21 02:14:46.243Z | 310.07° NW | 2026-06-21 02:16:46.243Z | 132.27° SE | 44.495° | 2026-06-21 02:19:46.243Z | 131.155° SE |
| 5 mins | 2026-06-21 19:06:46.243Z | 228.164° WSW | 2026-06-21 19:08:46.243Z | 223.753° SW | 43.609° | 2026-06-21 19:11:46.243Z | 50.444° ENE |
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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