DRAGON FREEDOM-2 DEB, 63331 (Decayed)
Orbit data source: Space-Track
DRAGON FREEDOM-2 DEB, 63331 was space debris in LEO originally from a launch on Sat, 28 Sep 2024 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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63331 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Decayed spacecraft
Bus & Motor
DRAGON SM, Unknown motor
Mass
Wet unknown, ~2,300 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.9 m
Radar Cross Section
16.128 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 DRAGON FREEDOM-2 DEB
1 63331U 24178B 25083.81891060 .19199630 12502-4 42883-3 0 9999
2 63331 52.1202 2.6839 0028753 88.5024 14.3950 16.43181485 968Epoch: 2025-03-24T19:39Z
TLE epoch observation values (Epoch: 2025-03-24T19:39:13.875Z)
Latitude
50.43508°
Longitude
-4.05518°
Altitude
144.908 km
Speed
7.837 km/s
True Right ascension
07h 33m 07s
True Declination
50° 15' 01"
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
20:46:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.591 km
Perigee altitude
139.006 km
Semi-major axis
6,535.935 km
Eccentricity
0.00288
Inclination
52.1202°
RAAN
2.6839°
Arg. of periapsis
88.5024°
True anomaly
14.4772°
Mean anomaly
14.395°
Eccentric anomaly
14.43607°
Mean motion
4.10754 °/min
Orbital period
87.64 mins
BSTAR
0.00042883
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Other satellites on launch #178 in the year 2024 (2024-09-28 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 FREEDOM-2 DEB 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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