STARLINK-36100, 66942
Orbit data source: Space-Track
STARLINK-36100, 66942 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 07 Dec 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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66942 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-36100
1 66942U 25286T 26171.44865199 .00027873 00000-0 83255-3 0 9996
2 66942 53.1603 240.1525 0001412 82.5137 277.6026 15.34417571 31091Epoch: 2026-06-20T10:46Z
TLE epoch observation values (Epoch: 2026-06-20T10:46:03.531Z)
Latitude
-0.00004°
Longitude
169.97463°
Altitude
463.425 km
Speed
7.636 km/s
True Right ascension
16h 00m 36s
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
07:15:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.874 km
Perigee altitude
461.942 km
Semi-major axis
6,841.045 km
Eccentricity
0.00014
Inclination
53.1603°
RAAN
240.1525°
Arg. of periapsis
82.5137°
True anomaly
277.58656°
Mean anomaly
277.6026°
Eccentric anomaly
277.59458°
Mean motion
3.83583 °/min
Orbital period
93.85 mins
BSTAR
0.00083255
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Other satellites on launch #286 in the year 2025 (2025-12-07 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-36100 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 | 2026-06-21 07:16:14.803Z | 226.8° WSW | 2026-06-21 07:19:14.803Z | 80.235° E | 44.615° | 2026-06-21 07:22:14.803Z | 51.16° ENE |
| 5 mins | 2026-06-21 13:51:14.803Z | 321.134° NNW | 2026-06-21 13:53:14.803Z | 67.621° E | 42.301° | 2026-06-21 13:56:14.803Z | 121.658° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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