ATLAS 5 CENTAUR DEB, 44664
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 44664 is space debris in HEO originally from a launch on Wed, 17 Oct 2018 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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44664 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ULA Decatur
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ATLAS 5 CENTAUR DEB
1 44664U 18079AA 24190.17350872 -.00000110 00000-0 00000-0 0 9991
2 44664 10.2312 125.1662 5129895 148.4729 256.1913 1.69334433 17227Epoch: 2024-07-08T04:09Z
TLE epoch observation values (Epoch: 2024-07-08T04:09:51.153Z)
Latitude
0.00001°
Longitude
135.95587°
Altitude
32,616.813 km
Speed
2.653 km/s
True Right ascension
08h 20m 07s
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
16:48:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,610.941 km
Perigee altitude
8,103.228 km
Semi-major axis
29,735.221 km
Eccentricity
0.51299
Inclination
10.2312°
RAAN
125.1662°
Arg. of periapsis
148.4729°
True anomaly
211.44796°
Mean anomaly
256.1913°
Eccentric anomaly
232.78442°
Mean motion
0.42329 °/min
Orbital period
850.48 mins
BSTAR
0
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Other satellites on launch #79 in the year 2018 (2018-10-17 UTC)
ATLAS 5 CENTAUR 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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