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
Last TLE update
7 hours ago
Origin
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

TLE from 7 hours ago
0 ATLAS CENTAUR 2 R/B
1   694U 63047A   25199.02066832  .00001580  00000-0  18148-3 0  9991
2   694  30.3552  65.8584 0552442 174.1119 186.6312 14.10894362 98069
Epoch: 2025-07-18T00:29Z
TLE epoch observation values (Epoch: 2025-07-18T00:29:45.742Z)
Latitude
0.00001°
Longitude
122.3397°
Altitude
1,251.979 km
Speed
7.031 km/s
True Right ascension
04h 23m 26s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
21.90497°
Longitude
-102.45053°
Altitude
557.615 km
Speed
7.741 km/s
Apparent Right ascension
11h 24m 39s
Apparent Declination
-9° 10' 09"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:40:55
Azimuth
298.851° NW
Elevation
-42.398°
Doppler factor
1
Orbital elements
Apogee altitude
1,259.962 km
Perigee altitude
460.221 km
Semi-major axis
7,238.229 km
Eccentricity
0.05524
Inclination
30.3552°
RAAN
65.8584°
Arg. of periapsis
174.1119°
True anomaly
185.94721°
Mean anomaly
186.6312°
Eccentric anomaly
186.2847°
Mean motion
3.52448 °/min
Orbital period
102.14 mins
BSTAR
0.00018148
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