STARLINK-37082, 68182
Orbit data source: Space-Track
STARLINK-37082, 68182 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 14 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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68182 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-37082
1 68182U 26050R 26171.31878529 .00020870 00000-0 62738-3 0 9994
2 68182 53.1585 148.8126 0001170 81.0875 279.0260 15.34386040 16414Epoch: 2026-06-20T07:39Z
TLE epoch observation values (Epoch: 2026-06-20T07:39:03.049Z)
Latitude
0°
Longitude
125.51478°
Altitude
463.52 km
Speed
7.636 km/s
True Right ascension
09h 55m 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
07:21:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.802 km
Perigee altitude
462.201 km
Semi-major axis
6,841.139 km
Eccentricity
0.00012
Inclination
53.1585°
RAAN
148.8126°
Arg. of periapsis
81.0875°
True anomaly
279.01276°
Mean anomaly
279.026°
Eccentric anomaly
279.01938°
Mean motion
3.83575 °/min
Orbital period
93.85 mins
BSTAR
0.00062738
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Other satellites on launch #50 in the year 2026 (2026-03-14 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-37082 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 01:00:46.641Z | 217.3° SW | 2026-06-21 01:03:46.641Z | 163.669° S | 40.926° | 2026-06-21 01:06:46.641Z | 58.187° ENE |
| 5 mins | 2026-06-21 07:35:46.641Z | 326.146° NNW | 2026-06-21 07:37:46.641Z | 24.885° NE | 37.912° | 2026-06-21 07:40:46.641Z | 110.73° ESE |
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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