STARLINK-35297, 66010
Orbit data source: Space-Track
STARLINK-35297, 66010 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 16 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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66010 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-35297
1 66010U 25232F 26171.20986251 .00000161 00000-0 15909-4 0 9993
2 66010 53.1618 346.8756 0001255 109.1638 250.9500 15.34404993 39138Epoch: 2026-06-20T05:02Z
TLE epoch observation values (Epoch: 2026-06-20T05:02:12.120Z)
Latitude
-0.00009°
Longitude
2.89727°
Altitude
463.87 km
Speed
7.636 km/s
True Right ascension
23h 07m 30s
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
07:23:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.804 km
Perigee altitude
462.086 km
Semi-major axis
6,841.082 km
Eccentricity
0.00013
Inclination
53.1618°
RAAN
346.8756°
Arg. of periapsis
109.1638°
True anomaly
250.93641°
Mean anomaly
250.95°
Eccentric anomaly
250.9432°
Mean motion
3.8358 °/min
Orbital period
93.85 mins
BSTAR
0.000015909
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Other satellites on launch #232 in the year 2025 (2025-10-16 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-35297 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 21:09:14.911Z | 313.936° NW | 2026-06-20 21:12:14.911Z | 347.314° N | 41.059° | 2026-06-20 21:16:14.911Z | 123.354° SE |
| 5 mins | 2026-06-21 14:03:14.911Z | 215.434° SW | 2026-06-21 14:05:14.911Z | 139.41° SSE | 42.858° | 2026-06-21 14:08:14.911Z | 55.765° ENE |
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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