STARLINK-35430, 66020
Orbit data source: Space-Track
STARLINK-35430, 66020 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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66020 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: 9 hours ago
TLE from 9 hours ago
0 STARLINK-35430
1 66020U 25232R 26171.47680797 .00002239 00000-0 87728-4 0 9995
2 66020 53.1610 346.4094 0001503 81.7006 278.4165 15.30194829 39156Epoch: 2026-06-20T11:26Z
TLE epoch observation values (Epoch: 2026-06-20T11:26:36.208Z)
Latitude
-0.00004°
Longitude
-93.93237°
Altitude
475.98 km
Speed
7.629 km/s
True Right ascension
23h 05m 38s
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
07:19:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.517 km
Perigee altitude
474.457 km
Semi-major axis
6,853.624 km
Eccentricity
0.00015
Inclination
53.161°
RAAN
346.4094°
Arg. of periapsis
81.7006°
True anomaly
278.39946°
Mean anomaly
278.4165°
Eccentric anomaly
278.40798°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000087728
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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-35430 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 21:20:54.838Z | 311.522° NW | 2026-06-20 21:23:54.838Z | 57.685° ENE | 44.843° | 2026-06-20 21:26:54.838Z | 128.448° SE |
| 6 mins | 2026-06-21 14:16:54.838Z | 227.593° WSW | 2026-06-21 14:18:54.838Z | 221.844° SW | 43.038° | 2026-06-21 14:22:54.838Z | 50.637° ENE |
| 4 mins | 2026-06-21 19:13:54.838Z | 343.657° N | 2026-06-21 19:15:54.838Z | 19.459° NNE | 15.881° | 2026-06-21 19:17:54.838Z | 55.626° 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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