STARLINK-32940, 63568
Orbit data source: Space-Track
STARLINK-32940, 63568 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 13 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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63568 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-32940
1 63568U 25075W 26171.38253604 .00012844 00000-0 47529-3 0 9994
2 63568 43.0057 50.5865 0000431 295.4964 64.5843 15.27590103 67630Epoch: 2026-06-20T09:10Z
TLE epoch observation values (Epoch: 2026-06-20T09:10:51.113Z)
Latitude
-0.00004°
Longitude
4.27552°
Altitude
482.668 km
Speed
7.626 km/s
True Right ascension
03h 22m 20s
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
08:42:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.259 km
Perigee altitude
484.667 km
Semi-major axis
6,863.1 km
Eccentricity
0.00004
Inclination
43.0057°
RAAN
50.5865°
Arg. of periapsis
295.4964°
True anomaly
64.58876°
Mean anomaly
64.5843°
Eccentric anomaly
64.58653°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00047529
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Other satellites on launch #75 in the year 2025 (2025-04-13 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-32940 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 22:04:04.573Z | 283.191° WNW | 2026-06-20 22:07:04.573Z | 346.44° N | 37.746° | 2026-06-20 22:10:04.573Z | 72.329° E |
| 6 mins | 2026-06-20 23:44:04.573Z | 290.609° WNW | 2026-06-20 23:46:04.573Z | 313.591° NW | 43.229° | 2026-06-20 23:50:04.573Z | 104.431° ESE |
| 5 mins | 2026-06-21 01:23:04.573Z | 259.665° W | 2026-06-21 01:25:04.573Z | 214.777° SW | 24.42° | 2026-06-21 01:28:04.573Z | 156.024° SSE |
| 4 mins | 2026-06-21 18:20:04.573Z | 180.417° SSW | 2026-06-21 18:22:04.573Z | 137.048° SSE | 19.869° | 2026-06-21 18:24:04.573Z | 100.352° ESE |
| 6 mins | 2026-06-21 19:58:04.573Z | 248.977° W | 2026-06-21 20:00:04.573Z | 239.473° WSW | 44.032° | 2026-06-21 20:04:04.573Z | 72.243° E |
| 6 mins | 2026-06-21 21:37:04.573Z | 287.602° WNW | 2026-06-21 21:39:04.573Z | 333.051° NNW | 36.829° | 2026-06-21 21:43:04.573Z | 75.799° E |
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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