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
Civil Technology
Bus & Motor
AC R&D, Unknown motor
Mass
4,300 kg wet, 900 kg dry
Launch date (UTC)
1963-11-27 (62 years ago)
Launch vehicle
ATLAS CENTAUR
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Nozzle, 4.3 m
Radar Cross Section
24.688 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 ATLAS CENTAUR 2 R/B
1 00694U 63047A   25259.22899967  .00001293  00000-0  14720-3 0  9996
2 00694  30.3553  89.9656 0551904 343.7863  14.5703 14.11043694106955
Epoch: 2025-09-16T05:29Z
TLE epoch observation values (Epoch: 2025-09-16T05:29:45.571Z)
Latitude
-0°
Longitude
12.10341°
Altitude
469.525 km
Speed
7.834 km/s
True Right ascension
05h 59m 51s
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
15:46:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,259.034 km
Perigee altitude
460.129 km
Semi-major axis
7,237.718 km
Eccentricity
0.05519
Inclination
30.3553°
RAAN
89.9656°
Arg. of periapsis
343.7863°
True anomaly
16.27452°
Mean anomaly
14.5703°
Eccentric anomaly
15.4106°
Mean motion
3.52485 °/min
Orbital period
102.13 mins
BSTAR
0.0001472
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