STARLINK-35395, 66014
Orbit data source: Space-Track
STARLINK-35395, 66014 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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66014 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: 18 hours ago
TLE from 18 hours ago
0 STARLINK-35395
1 66014U 25232K 26171.21239541 .00006110 00000-0 21818-3 0 9996
2 66014 53.1606 347.6009 0001258 99.9141 260.2002 15.30208982 39134Epoch: 2026-06-20T05:05Z
TLE epoch observation values (Epoch: 2026-06-20T05:05:50.963Z)
Latitude
-0°
Longitude
2.70829°
Altitude
476.235 km
Speed
7.629 km/s
True Right ascension
23h 10m 24s
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
10:19:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.307 km
Perigee altitude
474.582 km
Semi-major axis
6,853.582 km
Eccentricity
0.00013
Inclination
53.1606°
RAAN
347.6009°
Arg. of periapsis
99.9141°
True anomaly
260.186°
Mean anomaly
260.2002°
Eccentric anomaly
260.1931°
Mean motion
3.82531 °/min
Orbital period
94.11 mins
BSTAR
0.00021818
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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-35395 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 14:11:25.949Z | 224.247° SW | 2026-06-21 14:14:25.949Z | 173.468° S | 44.233° | 2026-06-21 14:17:25.949Z | 52.995° ENE |
| 4 mins | 2026-06-21 15:51:25.949Z | 306.542° NW | 2026-06-21 15:52:25.949Z | 326.917° NNW | 18.235° | 2026-06-21 15:55:25.949Z | 23.308° NE |
| 5 mins | 2026-06-21 20:47:25.949Z | 320.045° NNW | 2026-06-21 20:49:25.949Z | 16.418° NNE | 41.899° | 2026-06-21 20:52:25.949Z | 118.592° SE |
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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