ATLAS CENTAUR 2 DEB, 3741

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 3741 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 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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Identifier
3741, 1963-047L
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1963-11-27 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 03741U 63047L   26124.72233239  .00003919  00000-0  73749-3 0  9996
2 03741  29.8798 271.5091 0237624 281.5981  75.8038 14.46110171906500
Epoch: 2026-05-04T17:20Z
TLE epoch observation values (Epoch: 2026-05-04T17:20:09.518Z)
Latitude
-0°
Longitude
148.86199°
Altitude
699.174 km
Speed
7.529 km/s
True Right ascension
18h 06m 02s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
06:28:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
911.474 km
Perigee altitude
573.077 km
Semi-major axis
7,120.413 km
Eccentricity
0.02376
Inclination
29.8798°
RAAN
271.5091°
Arg. of periapsis
281.5981°
True anomaly
78.46203°
Mean anomaly
75.8038°
Eccentric anomaly
77.13109°
Mean motion
3.61231 °/min
Orbital period
99.66 mins
BSTAR
0.00073749
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