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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Edit Public Description
Expand to show TLE details & historyLast 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 14.11792095120382Epoch: 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
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
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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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 | 2025-12-22 00:02:19.666Z | 209.486° SW | 2025-12-22 00:04:19.666Z | 173.576° S | 18.036° | 2025-12-22 00:06:19.666Z | 137.059° 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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