ATLAS CENTAUR 2 R/B, 694

Orbit data source: Space-Track

ATLAS CENTAUR 2 R/B, 694 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 UTC via an ATLAS CENTAUR launch vehicle 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
694, 1963-047A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
AC R&D, Unknown motor
Mass
4,300 kg wet, 900 kg dry
Launch date (UTC)
1963-11-27 (63 years ago)
Launch vehicle
ATLAS CENTAUR
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 0.8 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 ATLAS CENTAUR 2 R/B
1 00694U 63047A   26227.64494533  .00000694  00000-0  74088-4 0  9996
2 00694  30.3546  26.8566 0545496  41.8956 322.2098 14.12603173154117
Epoch: 2026-08-15T15:28Z
TLE epoch observation values (Epoch: 2026-08-15T15:28:43.276Z)
Latitude
-0.00001°
Longitude
-169.37658°
Altitude
546.064 km
Speed
7.748 km/s
True Right ascension
01h 47m 25s
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
13:18:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,248.783 km
Perigee altitude
459.735 km
Semi-major axis
7,232.396 km
Eccentricity
0.05455
Inclination
30.3546°
RAAN
26.8566°
Arg. of periapsis
41.8956°
True anomaly
318.16517°
Mean anomaly
322.2098°
Eccentric anomaly
320.20956°
Mean motion
3.52874 °/min
Orbital period
102.02 mins
BSTAR
0.000074088
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