STARLINK-37054, 68082
Orbit data source: Space-Track
STARLINK-37054, 68082 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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68082 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 + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-37054
1 68082U 26042P 26228.21285171 .00011447 00000-0 34940-3 0 9995
2 68082 53.1575 154.5637 0001247 84.2308 275.8836 15.34401190 26771Epoch: 2026-08-16T05:06Z
TLE epoch observation values (Epoch: 2026-08-16T05:06:30.387Z)
Latitude
-0.00009°
Longitude
113.32441°
Altitude
463.513 km
Speed
7.636 km/s
True Right ascension
10h 18m 15s
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
12:16:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.81 km
Perigee altitude
462.104 km
Semi-major axis
6,841.094 km
Eccentricity
0.00012
Inclination
53.1575°
RAAN
154.5637°
Arg. of periapsis
84.2308°
True anomaly
275.86939°
Mean anomaly
275.8836°
Eccentric anomaly
275.87649°
Mean motion
3.83579 °/min
Orbital period
93.85 mins
BSTAR
0.0003494
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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-37054 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 | 2026-08-16 22:30:15.077Z | 252.948° W | 2026-08-16 22:33:15.077Z | 313.763° NW | 34.317° | 2026-08-16 22:36:15.077Z | 35.296° NE |
| 4 mins | 2026-08-17 03:28:15.077Z | 355.754° N | 2026-08-17 03:29:15.077Z | 20.053° NNE | 21.718° | 2026-08-17 03:32:15.077Z | 80.659° E |
| 5 mins | 2026-08-17 05:05:15.077Z | 292.486° WNW | 2026-08-17 05:07:15.077Z | 229.108° WSW | 37.823° | 2026-08-17 05:10:15.077Z | 150.51° SSE |
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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