STARLINK-36973, 68078
Orbit data source: Space-Track
STARLINK-36973, 68078 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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68078 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-36973
1 68078U 26042K 26171.41003435 .00021988 00000-0 66050-3 0 9998
2 68078 53.1594 60.0659 0001214 93.4820 266.6322 15.34376433 18058Epoch: 2026-06-20T09:50Z
TLE epoch observation values (Epoch: 2026-06-20T09:50:26.967Z)
Latitude
0°
Longitude
3.82848°
Altitude
463.723 km
Speed
7.636 km/s
True Right ascension
04h 00m 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
07:21:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.861 km
Perigee altitude
462.2 km
Semi-major axis
6,841.167 km
Eccentricity
0.00012
Inclination
53.1594°
RAAN
60.0659°
Arg. of periapsis
93.482°
True anomaly
266.61831°
Mean anomaly
266.6322°
Eccentric anomaly
266.62526°
Mean motion
3.83573 °/min
Orbital period
93.85 mins
BSTAR
0.0006605
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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-36973 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 | 2026-06-20 21:03:13.602Z | 302.838° NW | 2026-06-20 21:05:13.602Z | 344.661° N | 17.714° | 2026-06-20 21:07:13.602Z | 20.543° NNE |
| 5 mins | 2026-06-21 01:59:13.602Z | 324.686° NNW | 2026-06-21 02:01:13.602Z | 78.833° E | 40.36° | 2026-06-21 02:04:13.602Z | 120.521° SE |
| 5 mins | 2026-06-21 18:51:13.602Z | 212.123° SW | 2026-06-21 18:53:13.602Z | 150.992° SSE | 41.248° | 2026-06-21 18:56:13.602Z | 58.003° ENE |
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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