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.
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
694 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
Edit Public Description
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ATLAS CENTAUR 2 R/B
1 694U 63047A 25312.70913032 .00005568 00000-0 67714-3 0 9999
2 694 30.3502 151.4968 0550115 94.4783 271.8838 14.11424142114513Epoch: 2025-11-08T17:01Z
TLE epoch observation values (Epoch: 2025-11-08T17:01:08.859Z)
Latitude
-0.00003°
Longitude
-151.92502°
Altitude
861.808 km
Speed
7.419 km/s
True Right ascension
10h 05m 59s
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
21:51:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,256.369 km
Perigee altitude
460.196 km
Semi-major axis
7,236.42 km
Eccentricity
0.05501
Inclination
30.3502°
RAAN
151.4968°
Arg. of periapsis
94.4783°
True anomaly
265.58181°
Mean anomaly
271.8838°
Eccentric anomaly
268.73264°
Mean motion
3.5258 °/min
Orbital period
102.1 mins
BSTAR
0.00067714
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #47 in the year 1963 (1963-11-27 UTC)
Did you know?
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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| ATLAS CENTAUR 2 R/B is likely not visible in the next few days. |
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 ascending order |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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 ascending order |
|---|