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: 16 hours ago

TLE from 16 hours ago
0 ATLAS CENTAUR 2 R/B
1 00694U 63047A   26004.49070578  .00002491  00000-0  29044-3 0  9999
2 00694  30.3550 194.3639 0548723 234.6161 120.1977 14.11866353122543
Epoch: 2026-01-04T11:46Z
TLE epoch observation values (Epoch: 2026-01-04T11:46:36.979Z)
Latitude
-0.00001°
Longitude
-86.39166°
Altitude
1,066.608 km
Speed
7.211 km/s
True Right ascension
12h 57m 27s
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
03:31:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,253.769 km
Perigee altitude
459.776 km
Semi-major axis
7,234.909 km
Eccentricity
0.05487
Inclination
30.355°
RAAN
194.3639°
Arg. of periapsis
234.6161°
True anomaly
125.44353°
Mean anomaly
120.1977°
Eccentric anomaly
122.83923°
Mean motion
3.5269 °/min
Orbital period
102.07 mins
BSTAR
0.00029044
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