STARLINK-36954, 68057
Orbit data source: Space-Track
STARLINK-36954, 68057 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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68057 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 STARLINK-36954
1 68057U 26041T 26105.25002315 -.01925053 00000-0 -31931-1 0 9996
2 68057 53.1598 240.4172 0000722 90.3130 165.7420 15.55076783 5946Epoch: 2026-04-15T06:00Z
TLE epoch observation values (Epoch: 2026-04-15T06:00:02.000Z)
Latitude
-51.12854°
Longitude
-165.44958°
Altitude
420.089 km
Speed
7.659 km/s
True Right ascension
08h 31m 53s
True Declination
-50° 57' 07"
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
19:37:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
402.678 km
Perigee altitude
401.699 km
Semi-major axis
6,780.326 km
Eccentricity
0.00007
Inclination
53.1598°
RAAN
240.4172°
Arg. of periapsis
90.313°
True anomaly
165.74404°
Mean anomaly
165.742°
Eccentric anomaly
165.74302°
Mean motion
3.88747 °/min
Orbital period
92.61 mins
BSTAR
-0.031931
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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-36954 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-15 17:43:24.334Z | 339.973° N | 2026-04-15 17:45:24.334Z | 32.297° NE | 24.483° | 2026-04-15 17:47:24.334Z | 82.45° E |
| 4 mins | 2026-04-15 19:20:24.334Z | 271.585° WNW | 2026-04-15 19:21:24.334Z | 242.261° WSW | 26.805° | 2026-04-15 19:24:24.334Z | 165.302° S |
| 4 mins | 2026-04-16 12:01:24.334Z | 263.861° W | 2026-04-16 12:03:24.334Z | 352.929° N | 34.024° | 2026-04-16 12:05:24.334Z | 35.528° NE |
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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