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: 2 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   25321.81097159  .00001205  00000-0  42028-3 0  9993
2 00698  29.9241 358.7032 0530599 175.3071 185.2744 13.73816874 49962
Epoch: 2025-11-17T19:27Z
TLE epoch observation values (Epoch: 2025-11-17T19:27:47.945Z)
Latitude
-0.00002°
Longitude
9.64734°
Altitude
1,373.54 km
Speed
6.983 km/s
True Right ascension
23h 54m 48s
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
12:50:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,380.605 km
Perigee altitude
598.735 km
Semi-major axis
7,367.807 km
Eccentricity
0.05306
Inclination
29.9241°
RAAN
358.7032°
Arg. of periapsis
175.3071°
True anomaly
184.75018°
Mean anomaly
185.2744°
Eccentric anomaly
185.00896°
Mean motion
3.43191 °/min
Orbital period
104.9 mins
BSTAR
0.00042028
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