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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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: 18 hours ago
TLE from 18 hours ago
0 STARLINK-35592
1 66136U 25237Y 26061.44597374 .00028991 00000-0 98701-3 0 9996
2 66136 53.1586 73.1156 0001141 83.6036 276.5094 15.30204526 21507Epoch: 2026-03-02T10:42Z
TLE epoch observation values (Epoch: 2026-03-02T10:42:12.131Z)
Latitude
-0.00006°
Longitude
112.32574°
Altitude
476.013 km
Speed
7.629 km/s
True Right ascension
04h 52m 27s
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
08:40:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.24 km
Perigee altitude
474.676 km
Semi-major axis
6,853.595 km
Eccentricity
0.00011
Inclination
53.1586°
RAAN
73.1156°
Arg. of periapsis
83.6036°
True anomaly
276.49641°
Mean anomaly
276.5094°
Eccentric anomaly
276.5029°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.00098701
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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 | 2026-03-03 09:08:03.002Z | 356.506° N | 2026-03-03 09:09:03.002Z | 23.083° NE | 24.25° | 2026-03-03 09:12:03.002Z | 85.352° E |
| 5 mins | 2026-03-03 10:45:03.002Z | 288.567° WNW | 2026-03-03 10:47:03.002Z | 235.443° WSW | 33.928° | 2026-03-03 10:50:03.002Z | 157.699° S |
| 5 mins | 2026-03-04 03:41:03.002Z | 267.019° W | 2026-03-04 03:43:03.002Z | 342.097° N | 34.51° | 2026-03-04 03:46:03.002Z | 38.633° 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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