STARLINK-33666, 63592
Orbit data source: Space-Track
STARLINK-33666, 63592 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 14 Apr 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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63592 intel report (Beta)
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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 STARLINK-33666
1 63592U 25076Z 25302.81973775 .00029242 00000-0 10683-2 0 9993
2 63592 43.0015 340.9360 0000246 303.1287 56.9541 15.27569657 31817Epoch: 2025-10-29T19:40Z
TLE epoch observation values (Epoch: 2025-10-29T19:40:25.341Z)
Latitude
-0.00003°
Longitude
7.44299°
Altitude
482.764 km
Speed
7.626 km/s
True Right ascension
22h 43m 44s
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
00:15:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.194 km
Perigee altitude
484.856 km
Semi-major axis
6,863.162 km
Eccentricity
0.00002
Inclination
43.0015°
RAAN
340.936°
Arg. of periapsis
303.1287°
True anomaly
56.95646°
Mean anomaly
56.9541°
Eccentric anomaly
56.95528°
Mean motion
3.8173 °/min
Orbital period
94.31 mins
BSTAR
0.0010683
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Other satellites on launch #76 in the year 2025 (2025-04-14 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-33666 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-31 04:48:21.268Z | 184.708° SSW | 2025-10-31 04:50:21.268Z | 151.825° SSE | 16.444° | 2025-10-31 04:52:21.268Z | 113.174° SE |
| 5 mins | 2025-10-31 06:27:21.268Z | 239.815° WSW | 2025-10-31 06:29:21.268Z | 148.225° SSE | 44.008° | 2025-10-31 06:32:21.268Z | 74.409° E |
| 5 mins | 2025-10-31 08:06:21.268Z | 287.9° WNW | 2025-10-31 08:08:21.268Z | 354.545° N | 38.459° | 2025-10-31 08:11:21.268Z | 71.188° E |
| 5 mins | 2025-10-31 09:45:21.268Z | 293.35° NW | 2025-10-31 09:47:21.268Z | 344.559° N | 42.9° | 2025-10-31 09:50:21.268Z | 96.807° ESE |
| 5 mins | 2025-10-31 11:24:21.268Z | 263.002° W | 2025-10-31 11:26:21.268Z | 210.965° SW | 29.045° | 2025-10-31 11:29:21.268Z | 147.741° SSE |
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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