STARLINK-35679, 66408
Orbit data source: Space-Track
STARLINK-35679, 66408 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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66408 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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-35679
1 66408U 25257AE 26170.94701376 .00024817 00000-0 74294-3 0 9999
2 66408 53.1599 100.3335 0001333 96.5695 263.5459 15.34411211 35413Epoch: 2026-06-19T22:43Z
TLE epoch observation values (Epoch: 2026-06-19T22:43:41.988Z)
Latitude
-0.00007°
Longitude
-148.76019°
Altitude
463.674 km
Speed
7.636 km/s
True Right ascension
06h 41m 20s
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
08:33:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.839 km
Perigee altitude
462.015 km
Semi-major axis
6,841.064 km
Eccentricity
0.00013
Inclination
53.1599°
RAAN
100.3335°
Arg. of periapsis
96.5695°
True anomaly
263.53072°
Mean anomaly
263.5459°
Eccentric anomaly
263.53831°
Mean motion
3.83582 °/min
Orbital period
93.85 mins
BSTAR
0.00074294
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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-35679 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 22:22:25.485Z | 247.016° WSW | 2026-06-20 22:25:25.485Z | 328.047° NNW | 39.053° | 2026-06-20 22:28:25.485Z | 40.633° NE |
| 4 mins | 2026-06-21 03:19:25.485Z | 345.047° N | 2026-06-21 03:21:25.485Z | 27.095° NE | 19.45° | 2026-06-21 03:23:25.485Z | 67.365° ENE |
| 5 mins | 2026-06-21 04:57:25.485Z | 298.773° NW | 2026-06-21 04:59:25.485Z | 202.007° SSW | 42.241° | 2026-06-21 05:02:25.485Z | 141.143° SSE |
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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