STARLINK-35652, 66393
Orbit data source: Space-Track
STARLINK-35652, 66393 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 Nov 2025 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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66393 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-35652
1 66393U 25257P 26171.46191156 .00699657 00000-0 21019-1 0 9994
2 66393 53.1607 99.9942 0001703 58.3917 301.7250 15.31785595 35462Epoch: 2026-06-20T11:05Z
TLE epoch observation values (Epoch: 2026-06-20T11:05:09.158Z)
Latitude
-0.00008°
Longitude
25.02979°
Altitude
470.772 km
Speed
7.632 km/s
True Right ascension
06h 39m 58s
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
07:17:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.908 km
Perigee altitude
469.575 km
Semi-major axis
6,848.878 km
Eccentricity
0.00017
Inclination
53.1607°
RAAN
99.9942°
Arg. of periapsis
58.3917°
True anomaly
301.7084°
Mean anomaly
301.725°
Eccentric anomaly
301.7167°
Mean motion
3.82925 °/min
Orbital period
94.01 mins
BSTAR
0.021019
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Other satellites on launch #257 in the year 2025 (2025-11-08 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-35652 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 22:15:00.270Z | 237.133° WSW | 2026-06-20 22:17:00.270Z | 359.225° N | 44.028° | 2026-06-20 22:20:00.270Z | 47.271° ENE |
| 4 mins | 2026-06-21 03:11:00.270Z | 343.415° N | 2026-06-21 03:13:00.270Z | 20.439° NNE | 16.768° | 2026-06-21 03:15:00.270Z | 58.301° ENE |
| 5 mins | 2026-06-21 04:49:00.270Z | 312.075° NW | 2026-06-21 04:51:00.270Z | 330.841° NNW | 44.096° | 2026-06-21 04:54:00.270Z | 128.489° 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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