ATLAS CENTAUR 2 DEB, 698

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 698 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
698, 1963-047D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
CENTAUR PART, Unknown motor
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
Radar Cross Section
0.300 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   25242.81686327  .00001280  00000-0  44613-3 0  9991
2 00698  29.9256  54.3710 0531564 234.8652 120.0995 13.73684982 39090
Epoch: 2025-08-30T19:36Z
TLE epoch observation values (Epoch: 2025-08-30T19:36:16.986Z)
Latitude
-0.00003°
Longitude
141.05445°
Altitude
1,196.084 km
Speed
7.153 km/s
True Right ascension
03h 37m 29s
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
23:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,381.812 km
Perigee altitude
598.47 km
Semi-major axis
7,368.278 km
Eccentricity
0.05316
Inclination
29.9256°
RAAN
54.371°
Arg. of periapsis
234.8652°
True anomaly
125.19256°
Mean anomaly
120.0995°
Eccentric anomaly
122.66348°
Mean motion
3.43158 °/min
Orbital period
104.91 mins
BSTAR
0.00044613
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