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 (63 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: 10 hours ago

TLE from 10 hours ago
0 ATLAS CENTAUR 2 DEB
1   698U 63047D   26237.59362412  .00000364  00000-0  10944-3 0  9999
2   698  29.9235 320.1940 0528647   4.7523 355.7834 13.74417641 88613
Epoch: 2026-08-25T14:14Z
TLE epoch observation values (Epoch: 2026-08-25T14:14:49.123Z)
Latitude
-0.00002°
Longitude
132.63054°
Altitude
594.336 km
Speed
7.761 km/s
True Right ascension
21h 20m 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
15:52:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,376.908 km
Perigee altitude
598.141 km
Semi-major axis
7,365.662 km
Eccentricity
0.05286
Inclination
29.9235°
RAAN
320.194°
Arg. of periapsis
4.7523°
True anomaly
355.30666°
Mean anomaly
355.7834°
Eccentric anomaly
355.5483°
Mean motion
3.43341 °/min
Orbital period
104.85 mins
BSTAR
0.00010944
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