STARLINK-35424, 66460
Orbit data source: Space-Track
STARLINK-35424, 66460 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 15 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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66460 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-35424
1 66460U 25262E 26171.44859649 .00009141 00000-0 34120-3 0 9993
2 66460 43.0062 75.7077 0001542 268.6457 91.4218 15.27588581 34622Epoch: 2026-06-20T10:45Z
TLE epoch observation values (Epoch: 2026-06-20T10:45:58.736Z)
Latitude
-0.00004°
Longitude
5.54986°
Altitude
482.826 km
Speed
7.626 km/s
True Right ascension
05h 02m 49s
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
07:17:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.026 km
Perigee altitude
483.909 km
Semi-major axis
6,863.105 km
Eccentricity
0.00015
Inclination
43.0062°
RAAN
75.7077°
Arg. of periapsis
268.6457°
True anomaly
91.43946°
Mean anomaly
91.4218°
Eccentric anomaly
91.43063°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.0003412
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Other satellites on launch #262 in the year 2025 (2025-11-15 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-35424 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 | 2026-06-20 20:22:14.481Z | 186.113° SSW | 2026-06-20 20:24:14.481Z | 148.591° SSE | 19.113° | 2026-06-20 20:26:14.481Z | 107.951° ESE |
| 5 mins | 2026-06-20 22:01:14.481Z | 246.099° WSW | 2026-06-20 22:03:14.481Z | 97.335° ESE | 44.245° | 2026-06-20 22:06:14.481Z | 72.744° E |
| 5 mins | 2026-06-20 23:40:14.481Z | 291.818° WNW | 2026-06-20 23:42:14.481Z | 5.403° NNE | 38.033° | 2026-06-20 23:45:14.481Z | 73.147° E |
| 5 mins | 2026-06-21 01:19:14.481Z | 292.404° WNW | 2026-06-21 01:21:14.481Z | 1.139° NNE | 44.199° | 2026-06-21 01:24:14.481Z | 101.266° ESE |
| 5 mins | 2026-06-21 02:58:14.481Z | 257.28° W | 2026-06-21 03:00:14.481Z | 205.986° SW | 25.956° | 2026-06-21 03:03:14.481Z | 151.193° SSE |
| 4 mins | 2026-06-21 19:55:14.481Z | 173.881° S | 2026-06-21 19:56:14.481Z | 153.846° SSE | 18.409° | 2026-06-21 19:59:14.481Z | 98.499° 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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