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
Orbit
Country
USRelated business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
AC R&D, Unknown motor
Mass
4,300 kg wet, 900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ATLAS CENTAUR 2 R/B
1 00694U 63047A 26274.92039131 .00001877 00000-0 21847-3 0 9996
2 00694 30.3513 122.4076 0544723 98.9568 267.3065 14.12757632160800Epoch: 2026-10-01T22:05Z
TLE epoch observation values (Epoch: 2026-10-01T22:05:21.809Z)
Latitude
0.00002°
Longitude
140.417°
Altitude
888.228 km
Speed
7.39 km/s
True Right ascension
08h 09m 37s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:46:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,247.669 km
Perigee altitude
459.796 km
Semi-major axis
7,231.87 km
Eccentricity
0.05447
Inclination
30.3513°
RAAN
122.4076°
Arg. of periapsis
98.9568°
True anomaly
261.10336°
Mean anomaly
267.3065°
Eccentric anomaly
264.20144°
Mean motion
3.52913 °/min
Orbital period
102.01 mins
BSTAR
0.00021847
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Other satellites on launch #47 in the year 1963 (1963-11-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ATLAS CENTAUR 2 R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-02 18:44:09.291Z | 210.734° SW | 2026-10-02 18:46:09.291Z | 180.031° SSW | 16.74° | 2026-10-02 18:48:09.291Z | 142.64° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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