STARLINK-36853, 68097
Orbit data source: Space-Track
STARLINK-36853, 68097 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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68097 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
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-36853
1 68097U 26042AE 26132.02167554 .00016000 00000-0 48369-3 0 9998
2 68097 53.1594 244.4073 0000626 84.8806 275.2268 15.34397073 11995Epoch: 2026-05-12T00:31Z
TLE epoch observation values (Epoch: 2026-05-12T00:31:12.766Z)
Latitude
-0.00003°
Longitude
6.80205°
Altitude
463.574 km
Speed
7.636 km/s
True Right ascension
16h 17m 37s
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
17:52:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.397 km
Perigee altitude
462.541 km
Semi-major axis
6,841.106 km
Eccentricity
0.00006
Inclination
53.1594°
RAAN
244.4073°
Arg. of periapsis
84.8806°
True anomaly
275.21966°
Mean anomaly
275.2268°
Eccentric anomaly
275.22323°
Mean motion
3.83578 °/min
Orbital period
93.85 mins
BSTAR
0.00048369
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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-36853 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-12 10:03:39.984Z | 216.818° SW | 2026-05-12 10:07:39.984Z | 96.611° ESE | 38.771° | 2026-05-12 10:10:39.984Z | 56.525° ENE |
| 4 mins | 2026-05-12 11:43:39.984Z | 302.135° NW | 2026-05-12 11:44:39.984Z | 324.294° NNW | 19.985° | 2026-05-12 11:47:39.984Z | 24.322° NE |
| 5 mins | 2026-05-12 16:38:39.984Z | 324.887° NNW | 2026-05-12 16:40:39.984Z | 10.799° NNE | 36.273° | 2026-05-12 16:43:39.984Z | 108.113° 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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