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 (62 years ago)
Launch vehicle
ATLAS CENTAUR
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 ATLAS CENTAUR 2 R/B
1 00694U 63047A   25354.22011383  .00001631  00000-0  18952-3 0  9997
2 00694  30.3532 279.6750 0548805 100.0696 266.2251 14.11792095120382
Epoch: 2025-12-20T05:16Z
TLE epoch observation values (Epoch: 2025-12-20T05:16:57.834Z)
Latitude
-0.00004°
Longitude
111.38392°
Altitude
899.397 km
Speed
7.38 km/s
True Right ascension
18h 38m 41s
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
01:33:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,254.096 km
Perigee altitude
459.957 km
Semi-major axis
7,235.163 km
Eccentricity
0.05488
Inclination
30.3532°
RAAN
279.675°
Arg. of periapsis
100.0696°
True anomaly
259.99044°
Mean anomaly
266.2251°
Eccentric anomaly
263.10343°
Mean motion
3.52672 °/min
Orbital period
102.08 mins
BSTAR
0.00018952
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