STARLINK-35648, 66482
Orbit data source: Space-Track
STARLINK-35648, 66482 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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66482 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-35648
1 66482U 25262AC 26171.44988981 .00011785 00000-0 43700-3 0 9990
2 66482 42.9976 75.7105 0000760 37.8214 322.2691 15.27586471 34466Epoch: 2026-06-20T10:47Z
TLE epoch observation values (Epoch: 2026-06-20T10:47:50.479Z)
Latitude
-0.00002°
Longitude
5.08581°
Altitude
482.393 km
Speed
7.626 km/s
True Right ascension
05h 02m 50s
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
07:16:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.497 km
Perigee altitude
484.454 km
Semi-major axis
6,863.112 km
Eccentricity
0.00008
Inclination
42.9976°
RAAN
75.7105°
Arg. of periapsis
37.8214°
True anomaly
322.26377°
Mean anomaly
322.2691°
Eccentric anomaly
322.26644°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
0.000437
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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-35648 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 20:24:05.392Z | 188.197° SSW | 2026-06-20 20:26:05.392Z | 151.089° SSE | 19.482° | 2026-06-20 20:29:05.392Z | 96.118° ESE |
| 5 mins | 2026-06-20 22:03:05.392Z | 247.548° W | 2026-06-20 22:05:05.392Z | 104.537° ESE | 44.721° | 2026-06-20 22:08:05.392Z | 72.569° E |
| 5 mins | 2026-06-20 23:42:05.392Z | 291.015° WNW | 2026-06-20 23:44:05.392Z | 358.786° N | 38.086° | 2026-06-20 23:47:05.392Z | 72.951° E |
| 5 mins | 2026-06-21 01:21:05.392Z | 291.643° WNW | 2026-06-21 01:23:05.392Z | 340.064° N | 44.098° | 2026-06-21 01:26:05.392Z | 101.982° ESE |
| 5 mins | 2026-06-21 03:00:05.392Z | 258.049° W | 2026-06-21 03:02:05.392Z | 209.072° SW | 25.389° | 2026-06-21 03:05:05.392Z | 152.857° SSE |
| 4 mins | 2026-06-21 19:57:05.392Z | 176.216° S | 2026-06-21 19:59:05.392Z | 133.27° SE | 18.718° | 2026-06-21 20:01:05.392Z | 99.137° 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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