DRAGON CRS-32, 63628 (Decayed)
Orbit data source: Space-Track
DRAGON CRS-32, 63628 was a payload satellite owned by SpaceX (US) in LEO that was launched on Mon, 21 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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63628 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
None
Manufacturer
SpaceX
Mission
Decayed Commercial Spaceship
Bus & Motor
DRAGON CM, Unknown motor
Mass
~15,600 kg wet, ~9,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trunc Cone + Cyl + 2 Fin, 8.3 m
Radar Cross Section
36.564 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 DRAGON CRS-32
1 63628U 25080A 25143.97378780 .00207185 00000-0 31222-2 0 9999
2 63628 51.6379 67.0348 0003298 91.9939 7.7176 15.53535968 5191Epoch: 2025-05-23T23:22Z
TLE epoch observation values (Epoch: 2025-05-23T23:22:15.265Z)
Latitude
50.76583°
Longitude
-59.90894°
Altitude
410.013 km
Speed
7.672 km/s
True Right ascension
11h 29m 54s
True Declination
50° 35' 19"
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
10:52:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.158 km
Perigee altitude
404.683 km
Semi-major axis
6,785.058 km
Eccentricity
0.00033
Inclination
51.6379°
RAAN
67.0348°
Arg. of periapsis
91.9939°
True anomaly
7.72268°
Mean anomaly
7.7176°
Eccentric anomaly
7.72014°
Mean motion
3.88341 °/min
Orbital period
92.7 mins
BSTAR
0.0031222
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Other satellites on launch #80 in the year 2025 (2025-04-21 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.DRAGON CRS-32 Visibility
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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. |
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| This satellite is decayed. |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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