STARLINK-32958, 63563
Orbit data source: Space-Track
STARLINK-32958, 63563 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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63563 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32958
1 63563U 25075R 26171.38639513 .00019325 00000-0 70988-3 0 9992
2 63563 43.0025 50.6492 0000661 326.6558 33.4252 15.27582076 67637Epoch: 2026-06-20T09:16Z
TLE epoch observation values (Epoch: 2026-06-20T09:16:24.539Z)
Latitude
-0°
Longitude
2.94519°
Altitude
482.44 km
Speed
7.626 km/s
True Right ascension
03h 22m 35s
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
07:13:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.441 km
Perigee altitude
484.534 km
Semi-major axis
6,863.125 km
Eccentricity
0.00007
Inclination
43.0025°
RAAN
50.6492°
Arg. of periapsis
326.6558°
True anomaly
33.42937°
Mean anomaly
33.4252°
Eccentric anomaly
33.42729°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00070988
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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-32958 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 20:30:18.025Z | 252.327° W | 2026-06-20 20:34:18.025Z | 62.09° ENE | 43.646° | 2026-06-20 20:37:18.025Z | 71.547° E |
| 5 mins | 2026-06-20 22:11:18.025Z | 295.041° NW | 2026-06-20 22:13:18.025Z | 12.48° NNE | 37.692° | 2026-06-20 22:16:18.025Z | 75.341° E |
| 5 mins | 2026-06-20 23:50:18.025Z | 290.107° WNW | 2026-06-20 23:52:18.025Z | 40.802° NE | 44.867° | 2026-06-20 23:55:18.025Z | 106.26° ESE |
| 4 mins | 2026-06-21 01:29:18.025Z | 251.684° W | 2026-06-21 01:31:18.025Z | 203.668° SW | 22.487° | 2026-06-21 01:33:18.025Z | 164.87° S |
| 4 mins | 2026-06-21 18:26:18.025Z | 175.092° S | 2026-06-21 18:27:18.025Z | 151.818° SSE | 21.478° | 2026-06-21 18:30:18.025Z | 94.314° ESE |
| 5 mins | 2026-06-21 20:04:18.025Z | 252.382° W | 2026-06-21 20:06:18.025Z | 56.403° ENE | 44.821° | 2026-06-21 20:09:18.025Z | 71.633° 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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