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 shape, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ATLAS CENTAUR 2 DEB
1   698U 63047D   26119.99077170  .00000653  00000-0  21798-3 0  9996
2   698  29.9200 219.5950 0529055 100.4539 265.6075 13.74228989 72425
Epoch: 2026-04-29T23:46Z
TLE epoch observation values (Epoch: 2026-04-29T23:46:42.674Z)
Latitude
-0.00005°
Longitude
4.9733°
Altitude
1,033.071 km
Speed
7.312 km/s
True Right ascension
14h 38m 22s
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
16:36:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,377.918 km
Perigee altitude
598.479 km
Semi-major axis
7,366.336 km
Eccentricity
0.05291
Inclination
29.92°
RAAN
219.595°
Arg. of periapsis
100.4539°
True anomaly
259.60425°
Mean anomaly
265.6075°
Eccentric anomaly
262.60147°
Mean motion
3.43294 °/min
Orbital period
104.87 mins
BSTAR
0.00021798
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