STARLINK-34022, 63866
Orbit data source: Space-Track
STARLINK-34022, 63866 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 10 May 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63866 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-34022
1 63866U 25094C 26171.45286536 .00007521 00000-0 63705-3 0 9994
2 63866 70.0014 335.4492 0002446 266.2592 93.8288 14.98355833 62590Epoch: 2026-06-20T10:52Z
TLE epoch observation values (Epoch: 2026-06-20T10:52:07.567Z)
Latitude
0.00005°
Longitude
-96.24959°
Altitude
574.514 km
Speed
7.574 km/s
True Right ascension
22h 21m 47s
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
07:18:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.624 km
Perigee altitude
568.225 km
Semi-major axis
6,948.061 km
Eccentricity
0.00024
Inclination
70.0014°
RAAN
335.4492°
Arg. of periapsis
266.2592°
True anomaly
93.85677°
Mean anomaly
93.8288°
Eccentric anomaly
93.84278°
Mean motion
3.74755 °/min
Orbital period
96.06 mins
BSTAR
0.00063705
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Other satellites on launch #94 in the year 2025 (2025-05-10 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-34022 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 21:01:38.773Z | 18.674° NNE | 2026-06-20 21:03:38.773Z | 52.281° ENE | 17.864° | 2026-06-20 21:06:38.773Z | 99.351° ESE |
| 6 mins | 2026-06-20 22:39:38.773Z | 310.213° NW | 2026-06-20 22:42:38.773Z | 235.333° WSW | 31.013° | 2026-06-20 22:45:38.773Z | 185.586° SSW |
| 6 mins | 2026-06-21 12:39:38.773Z | 225.814° WSW | 2026-06-21 12:41:38.773Z | 268.207° W | 38.122° | 2026-06-21 12:45:38.773Z | 13.783° NNE |
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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