STARLINK-34622, 66015
Orbit data source: Space-Track
STARLINK-34622, 66015 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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66015 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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-34622
1 66015U 25232L 26170.90311920 .00024377 00000-0 73003-3 0 9992
2 66015 53.1601 348.5178 0001037 79.6367 280.4753 15.34409895 39088Epoch: 2026-06-19T21:40Z
TLE epoch observation values (Epoch: 2026-06-19T21:40:29.498Z)
Latitude
0°
Longitude
115.26947°
Altitude
463.446 km
Speed
7.636 km/s
True Right ascension
23h 14m 04s
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
07:23:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.64 km
Perigee altitude
462.221 km
Semi-major axis
6,841.068 km
Eccentricity
0.0001
Inclination
53.1601°
RAAN
348.5178°
Arg. of periapsis
79.6367°
True anomaly
280.46361°
Mean anomaly
280.4753°
Eccentric anomaly
280.46946°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00073003
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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-34622 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 21:37:44.108Z | 303.279° NW | 2026-06-20 21:40:44.108Z | 248.378° W | 40.801° | 2026-06-20 21:43:44.108Z | 144.793° SSE |
| 5 mins | 2026-06-21 14:31:44.108Z | 246.87° WSW | 2026-06-21 14:33:44.108Z | 346.789° N | 41.684° | 2026-06-21 14:36:44.108Z | 44.227° NE |
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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