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: 7 hours ago

TLE from 7 hours ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   26065.28696901  .00000912  00000-0  31471-3 0  9994
2 00698  29.9213 147.6608 0529551   2.7564 357.5772 13.74182111 64896
Epoch: 2026-03-06T06:53Z
TLE epoch observation values (Epoch: 2026-03-06T06:53:14.122Z)
Latitude
Longitude
-119.67318°
Altitude
593.683 km
Speed
7.762 km/s
True Right ascension
09h 50m 38s
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
18:00:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,378.46 km
Perigee altitude
598.272 km
Semi-major axis
7,366.503 km
Eccentricity
0.05296
Inclination
29.9213°
RAAN
147.6608°
Arg. of periapsis
2.7564°
True anomaly
357.30257°
Mean anomaly
357.5772°
Eccentric anomaly
357.44177°
Mean motion
3.43282 °/min
Orbital period
104.87 mins
BSTAR
0.00031471
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