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   26003.96844049  .00003432  00000-0  12539-2 0  9992
2 00698  29.9241 110.5013 0529644 209.7749 147.1672 13.74003364 56450
Epoch: 2026-01-03T23:14Z
TLE epoch observation values (Epoch: 2026-01-03T23:14:33.258Z)
Latitude
0.00002°
Longitude
18.27607°
Altitude
1,317.021 km
Speed
7.036 km/s
True Right ascension
07h 22m 00s
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
05:52:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,379.2 km
Perigee altitude
598.807 km
Semi-major axis
7,367.141 km
Eccentricity
0.05296
Inclination
29.9241°
RAAN
110.5013°
Arg. of periapsis
209.7749°
True anomaly
150.28262°
Mean anomaly
147.1672°
Eccentric anomaly
148.74186°
Mean motion
3.43237 °/min
Orbital period
104.88 mins
BSTAR
0.0012539
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