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: 20 hours ago

TLE from 20 hours ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   26004.54960726  .00003078  00000-0  11206-2 0  9994
2 00698  29.9242 107.4425 0529673 214.6362 141.8611 13.74006348 56539
Epoch: 2026-01-04T13:11Z
TLE epoch observation values (Epoch: 2026-01-04T13:11:26.067Z)
Latitude
0.00001°
Longitude
165.42439°
Altitude
1,297.794 km
Speed
7.055 km/s
True Right ascension
07h 09m 46s
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
09:26:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,379.21 km
Perigee altitude
598.776 km
Semi-major axis
7,367.13 km
Eccentricity
0.05297
Inclination
29.9242°
RAAN
107.4425°
Arg. of periapsis
214.6362°
True anomaly
145.42135°
Mean anomaly
141.8611°
Eccentric anomaly
143.65947°
Mean motion
3.43238 °/min
Orbital period
104.88 mins
BSTAR
0.0011206
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