STARLINK-36857, 68518
Orbit data source: Space-Track
STARLINK-36857, 68518 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 30 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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68518 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, 2.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-36857
1 68518U 26068L 26170.84077575 .00021408 00000-0 64277-3 0 9993
2 68518 53.1586 12.7371 0000911 78.5403 281.5702 15.34407563 12610Epoch: 2026-06-19T20:10Z
TLE epoch observation values (Epoch: 2026-06-19T20:10:43.024Z)
Latitude
-0.00003°
Longitude
161.99384°
Altitude
463.457 km
Speed
7.636 km/s
True Right ascension
00h 50m 56s
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
07:20:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.561 km
Perigee altitude
462.315 km
Semi-major axis
6,841.075 km
Eccentricity
0.00009
Inclination
53.1586°
RAAN
12.7371°
Arg. of periapsis
78.5403°
True anomaly
281.55997°
Mean anomaly
281.5702°
Eccentric anomaly
281.56509°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00064277
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Other satellites on launch #68 in the year 2026 (2026-03-30 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-36857 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 21:38:37.861Z | 337.143° NNW | 2026-06-20 21:40:37.861Z | 14.253° NNE | 20.424° | 2026-06-20 21:43:37.861Z | 76.294° E |
| 5 mins | 2026-06-20 23:16:37.861Z | 297.245° NW | 2026-06-20 23:18:37.861Z | 248.579° W | 38.978° | 2026-06-20 23:21:37.861Z | 148.232° SSE |
| 5 mins | 2026-06-21 16:09:37.861Z | 250.232° W | 2026-06-21 16:11:37.861Z | 336.818° NNW | 40.676° | 2026-06-21 16:14:37.861Z | 42.662° 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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