STARLINK-36952, 68062
Orbit data source: Space-Track
STARLINK-36952, 68062 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 02 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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68062 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: 1 day ago
TLE from 1 day ago
0 STARLINK-36952
1 68062U 26041Y 26170.72361171 .00015524 00000-0 46949-3 0 9991
2 68062 53.1595 293.5695 0001055 88.4357 271.6767 15.34409642 17043Epoch: 2026-06-19T17:22Z
TLE epoch observation values (Epoch: 2026-06-19T17:22:00.051Z)
Latitude
0.00001°
Longitude
125.1208°
Altitude
463.555 km
Speed
7.636 km/s
True Right ascension
19h 34m 16s
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
07:20:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.653 km
Perigee altitude
462.21 km
Semi-major axis
6,841.069 km
Eccentricity
0.00011
Inclination
53.1595°
RAAN
293.5695°
Arg. of periapsis
88.4357°
True anomaly
271.66462°
Mean anomaly
271.6767°
Eccentric anomaly
271.67066°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00046949
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Other satellites on launch #41 in the year 2026 (2026-03-02 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-36952 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 10:10:52.127Z | 206.899° SW | 2026-06-21 10:13:52.127Z | 113.058° SE | 36.302° | 2026-06-21 10:16:52.127Z | 60.138° ENE |
| 4 mins | 2026-06-21 11:49:52.127Z | 297.346° NW | 2026-06-21 11:50:52.127Z | 320.513° NNW | 21.68° | 2026-06-21 11:53:52.127Z | 24.593° NE |
| 4 mins | 2026-06-21 16:45:52.127Z | 340.622° N | 2026-06-21 16:46:52.127Z | 10.899° NNE | 32.785° | 2026-06-21 16:49:52.127Z | 101.475° ESE |
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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