STARLINK-35862, 66628
Orbit data source: Space-Track
STARLINK-35862, 66628 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 23 Nov 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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66628 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 + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-35862
1 66628U 25271M 26218.55621004 .00017610 00000-0 53116-3 0 9991
2 66628 53.1583 160.1495 0001787 82.7038 277.4168 15.34395323 40560Epoch: 2026-08-06T13:20Z
TLE epoch observation values (Epoch: 2026-08-06T13:20:56.547Z)
Latitude
0.00001°
Longitude
4.81933°
Altitude
463.461 km
Speed
7.636 km/s
True Right ascension
10h 40m 35s
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
13:48:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.197 km
Perigee altitude
461.752 km
Semi-major axis
6,841.111 km
Eccentricity
0.00018
Inclination
53.1583°
RAAN
160.1495°
Arg. of periapsis
82.7038°
True anomaly
277.39649°
Mean anomaly
277.4168°
Eccentric anomaly
277.40665°
Mean motion
3.83578 °/min
Orbital period
93.85 mins
BSTAR
0.00053116
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Other satellites on launch #271 in the year 2025 (2025-11-23 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-35862 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 | 2026-08-07 00:33:17.254Z | 297.507° NW | 2026-08-07 00:35:17.254Z | 338.71° N | 18.62° | 2026-08-07 00:37:17.254Z | 17.69° NNE |
| 5 mins | 2026-08-07 05:29:17.254Z | 325.257° NNW | 2026-08-07 05:31:17.254Z | 52.376° ENE | 40.459° | 2026-08-07 05:34:17.254Z | 116.936° SE |
| 5 mins | 2026-08-07 22:21:17.254Z | 209.816° SW | 2026-08-07 22:23:17.254Z | 166.347° S | 38.213° | 2026-08-07 22:26:17.254Z | 61.323° ENE |
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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