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 (63 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.050 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 ATLAS CENTAUR 2 DEB
1 03741U 63047L   26301.34381183  .00001567  00000-0  27749-3 0  9999
2 03741  29.8779 306.8074 0232955 142.6216 219.0837 14.47549012932107
Epoch: 2026-10-28T08:15Z
TLE epoch observation values (Epoch: 2026-10-28T08:15:05.342Z)
Latitude
0.00002°
Longitude
146.34123°
Altitude
862.168 km
Speed
7.356 km/s
True Right ascension
20h 27m 13s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
16:51:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
903.325 km
Perigee altitude
571.798 km
Semi-major axis
7,115.699 km
Eccentricity
0.0233
Inclination
29.8779°
RAAN
306.8074°
Arg. of periapsis
142.6216°
True anomaly
217.43818°
Mean anomaly
219.0837°
Eccentric anomaly
218.25724°
Mean motion
3.6159 °/min
Orbital period
99.56 mins
BSTAR
0.00027749
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