STARLINK-35562, 66063
Orbit data source: Space-Track
STARLINK-35562, 66063 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 19 Oct 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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66063 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: 1 day ago
TLE from 1 day ago
0 STARLINK-35562
1 66063U 25235F 26170.62980015 .00017917 00000-0 61534-3 0 9992
2 66063 53.1595 132.1439 0001323 72.2141 287.9004 15.30212847 38521Epoch: 2026-06-19T15:06Z
TLE epoch observation values (Epoch: 2026-06-19T15:06:54.732Z)
Latitude
-0.00005°
Longitude
-2.44021°
Altitude
475.798 km
Speed
7.629 km/s
True Right ascension
08h 48m 34s
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
10:17:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.34 km
Perigee altitude
474.526 km
Semi-major axis
6,853.57 km
Eccentricity
0.00013
Inclination
53.1595°
RAAN
132.1439°
Arg. of periapsis
72.2141°
True anomaly
287.88597°
Mean anomaly
287.9004°
Eccentric anomaly
287.89319°
Mean motion
3.82532 °/min
Orbital period
94.11 mins
BSTAR
0.00061534
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Other satellites on launch #235 in the year 2025 (2025-10-19 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-35562 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 | 2026-06-21 00:13:40.079Z | 241.313° WSW | 2026-06-21 00:16:40.079Z | 347.794° N | 41.823° | 2026-06-21 00:19:40.079Z | 44.268° NE |
| 4 mins | 2026-06-21 05:11:40.079Z | 351.496° N | 2026-06-21 05:13:40.079Z | 34.101° NE | 18.105° | 2026-06-21 05:15:40.079Z | 68.769° E |
| 5 mins | 2026-06-21 06:49:40.079Z | 305.05° NW | 2026-06-21 06:51:40.079Z | 176.904° S | 44.084° | 2026-06-21 06:54:40.079Z | 135.474° 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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