STARLINK-35592, 66136
Orbit data source: Space-Track
STARLINK-35592, 66136 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 22 Oct 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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66136 intel report (Beta)
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Edit Public Description
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, 17.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 STARLINK-35592
1 66136U 25237Y 25311.83336806 -.01835142 00000-0 -15989-1 0 9999
2 66136 53.1597 253.0015 0001131 120.6841 109.6494 15.71659837 3860Epoch: 2025-11-07T20:00Z
TLE epoch observation values (Epoch: 2025-11-07T20:00:03.000Z)
Latitude
-38.2466°
Longitude
121.67826°
Altitude
366.85 km
Speed
7.689 km/s
True Right ascension
07h 15m 50s
True Declination
-38° 04' 11"
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
20:32:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
355.175 km
Perigee altitude
353.652 km
Semi-major axis
6,732.551 km
Eccentricity
0.00011
Inclination
53.1597°
RAAN
253.0015°
Arg. of periapsis
120.6841°
True anomaly
109.66161°
Mean anomaly
109.6494°
Eccentric anomaly
109.6555°
Mean motion
3.92892 °/min
Orbital period
91.63 mins
BSTAR
-0.015989
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Other satellites on launch #237 in the year 2025 (2025-10-22 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-35592 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 | 2025-11-08 06:14:10.691Z | 292.43° WNW | 2025-11-08 06:15:10.691Z | 264.044° W | 36.041° | 2025-11-08 06:18:10.691Z | 146.126° SSE |
| 4 mins | 2025-11-08 22:44:10.691Z | 217.399° SW | 2025-11-08 22:45:10.691Z | 162.688° S | 43.908° | 2025-11-08 22:48:10.691Z | 53.012° ENE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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