STARLINK-36308, 68543
Orbit data source: Space-Track
STARLINK-36308, 68543 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Apr 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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68543 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, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-36308
1 68543U 26070B 26145.34282357 .00017145 00000-0 51702-3 0 9999
2 68543 53.1609 6.3311 0000776 89.4748 270.6343 15.34423044 8290Epoch: 2026-05-25T08:13Z
TLE epoch observation values (Epoch: 2026-05-25T08:13:39.956Z)
Latitude
-0.00006°
Longitude
-0.01741°
Altitude
463.53 km
Speed
7.636 km/s
True Right ascension
00h 25m 19s
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
09:22:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.422 km
Perigee altitude
462.361 km
Semi-major axis
6,841.028 km
Eccentricity
0.00008
Inclination
53.1609°
RAAN
6.3311°
Arg. of periapsis
89.4748°
True anomaly
270.62541°
Mean anomaly
270.6343°
Eccentric anomaly
270.62985°
Mean motion
3.83585 °/min
Orbital period
93.85 mins
BSTAR
0.00051702
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Other satellites on launch #70 in the year 2026 (2026-04-02 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-36308 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 | 2026-05-26 00:21:26.668Z | 309.73° NW | 2026-05-26 00:24:26.668Z | 303.977° NW | 44.611° | 2026-05-26 00:27:26.668Z | 131.475° SE |
| 5 mins | 2026-05-26 17:15:26.668Z | 228.506° WSW | 2026-05-26 17:17:26.668Z | 52.606° ENE | 43.702° | 2026-05-26 17:20:26.668Z | 50.255° ENE |
| 5 mins | 2026-05-26 23:49:26.668Z | 320.577° NNW | 2026-05-26 23:51:26.668Z | 87.99° E | 41.707° | 2026-05-26 23:54:26.668Z | 123.535° SE |
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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