DRAGON CRS-31 DEB, 62608 (Decayed)
Orbit data source: Space-Track
DRAGON CRS-31 DEB, 62608 was space debris in LEO originally from a launch on Tue, 05 Nov 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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62608 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 DRAGON CRS-31 DEB
1 62608U 24200B 25029.65332789 .05515617 12458-4 39522-3 0 9999
2 62608 51.6226 259.7984 0005990 314.7115 89.5839 16.40053217 2479Epoch: 2025-01-29T15:40Z
TLE epoch observation values (Epoch: 2025-01-29T15:40:47.529Z)
Latitude
33.3542°
Longitude
-73.324°
Altitude
167.731 km
Speed
7.81 km/s
True Right ascension
19h 24m 03s
True Declination
33° 10' 56"
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
12:36:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
170.111 km
Perigee altitude
162.271 km
Semi-major axis
6,544.328 km
Eccentricity
0.0006
Inclination
51.6226°
RAAN
259.7984°
Arg. of periapsis
314.7115°
True anomaly
89.65254°
Mean anomaly
89.5839°
Eccentric anomaly
89.61822°
Mean motion
4.09964 °/min
Orbital period
87.81 mins
BSTAR
0.00039522
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Other satellites on launch #200 in the year 2024 (2024-11-05 UTC)
DRAGON CRS-31 DEB Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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