STARLINK-36375, 67920
Orbit data source: Space-Track
STARLINK-36375, 67920 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 22 Feb 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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67920 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-36375
1 67920U 26036S 26171.31655882 .00014504 00000-0 53536-3 0 9995
2 67920 43.0037 26.0215 0001861 271.7949 88.2689 15.27590775 19418Epoch: 2026-06-20T07:35Z
TLE epoch observation values (Epoch: 2026-06-20T07:35:50.682Z)
Latitude
-0.00004°
Longitude
3.52736°
Altitude
482.754 km
Speed
7.626 km/s
True Right ascension
01h 44m 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
07:23:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.239 km
Perigee altitude
483.684 km
Semi-major axis
6,863.098 km
Eccentricity
0.00019
Inclination
43.0037°
RAAN
26.0215°
Arg. of periapsis
271.7949°
True anomaly
88.29022°
Mean anomaly
88.2689°
Eccentric anomaly
88.27956°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00053536
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Other satellites on launch #36 in the year 2026 (2026-02-22 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-36375 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 | 2026-06-20 20:29:16.402Z | 284° WNW | 2026-06-20 20:32:16.402Z | 349.704° N | 37.845° | 2026-06-20 20:35:16.402Z | 73.1° E |
| 6 mins | 2026-06-20 22:09:16.402Z | 290.106° WNW | 2026-06-20 22:11:16.402Z | 310.804° NW | 43.732° | 2026-06-20 22:15:16.402Z | 105.717° ESE |
| 5 mins | 2026-06-20 23:48:16.402Z | 257.953° W | 2026-06-20 23:50:16.402Z | 213.267° SW | 23.536° | 2026-06-20 23:53:16.402Z | 157.027° SSE |
| 4 mins | 2026-06-21 16:45:16.402Z | 180.598° SSW | 2026-06-21 16:47:16.402Z | 135.285° SSE | 20.606° | 2026-06-21 16:49:16.402Z | 98.786° ESE |
| 5 mins | 2026-06-21 18:23:16.402Z | 250.772° W | 2026-06-21 18:25:16.402Z | 249.744° W | 44.399° | 2026-06-21 18:28:16.402Z | 71.874° E |
| 6 mins | 2026-06-21 20:02:16.402Z | 288.606° WNW | 2026-06-21 20:04:16.402Z | 336.272° NNW | 37.067° | 2026-06-21 20:08:16.402Z | 76.497° E |
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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