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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ATLAS CENTAUR 2 R/B
1 694U 63047A 26145.17092160 .00002546 00000-0 30113-3 0 9991
2 694 30.3516 128.1027 0546183 34.5354 328.9514 14.12433347142440Epoch: 2026-05-25T04:06Z
TLE epoch observation values (Epoch: 2026-05-25T04:06:07.626Z)
Latitude
-0°
Longitude
-176.19163°
Altitude
517.528 km
Speed
7.779 km/s
True Right ascension
08h 32m 24s
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
21:30:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,249.891 km
Perigee altitude
459.786 km
Semi-major axis
7,232.975 km
Eccentricity
0.05462
Inclination
30.3516°
RAAN
128.1027°
Arg. of periapsis
34.5354°
True anomaly
325.52538°
Mean anomaly
328.9514°
Eccentric anomaly
327.25888°
Mean motion
3.52832 °/min
Orbital period
102.03 mins
BSTAR
0.00030113
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-26 04:09:27.814Z | 217.701° SW | 2026-05-26 04:12:27.814Z | 164.529° S | 18.615° | 2026-05-26 04:14:27.814Z | 131.914° SE |
| 5 mins | 2026-05-26 05:57:27.814Z | 221.406° SW | 2026-05-26 05:59:27.814Z | 185.993° SSW | 20.589° | 2026-05-26 06:02:27.814Z | 141.909° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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