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 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-36853
1 68097U 26042AE 26070.41668981 -.01436458 64110-3 -27584-2 0 9998
2 68097 53.1595 186.3303 0000628 81.9099 254.3015 15.99904382 2323Epoch: 2026-03-11T10:00Z
TLE epoch observation values (Epoch: 2026-03-11T10:00:01.999Z)
Latitude
-19.0222°
Longitude
-147.6413°
Altitude
280.056 km
Speed
7.739 km/s
True Right ascension
11h 25m 47s
True Declination
-18° 54' 32"
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
02:06:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
275.366 km
Perigee altitude
274.53 km
Semi-major axis
6,653.085 km
Eccentricity
0.00006
Inclination
53.1595°
RAAN
186.3303°
Arg. of periapsis
81.9099°
True anomaly
254.29457°
Mean anomaly
254.3015°
Eccentric anomaly
254.29804°
Mean motion
3.99953 °/min
Orbital period
90.01 mins
BSTAR
-0.0027584
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-12 10:17:43.639Z | 229.612° WSW | 2026-03-12 10:19:43.639Z | 239.728° WSW | 44.834° | 2026-03-12 10:21:43.639Z | 49.586° ENE |
| 4 mins | 2026-03-12 16:35:43.639Z | 326.716° NNW | 2026-03-12 16:37:43.639Z | 37.529° NE | 32.049° | 2026-03-12 16:39:43.639Z | 105.789° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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