ATLAS CENTAUR 2 DEB, 700
Orbit data source: Space-Track
ATLAS CENTAUR 2 DEB, 700 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 UTC launched 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
CENTAUR PART, Unknown motor
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.7 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ATLAS CENTAUR 2 DEB
1 700U 63047F 26128.95194355 .00000281 00000-0 83918-4 0 9991
2 700 30.4784 226.7318 0716941 137.1941 228.6781 13.40184344 44866Epoch: 2026-05-08T22:50Z
TLE epoch observation values (Epoch: 2026-05-08T22:50:47.922Z)
Latitude
-0.00003°
Longitude
17.25572°
Altitude
1,481.714 km
Speed
6.945 km/s
True Right ascension
15h 06m 55s
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
22:18:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,649.255 km
Perigee altitude
575.223 km
Semi-major axis
7,490.376 km
Eccentricity
0.07169
Inclination
30.4784°
RAAN
226.7318°
Arg. of periapsis
137.1941°
True anomaly
222.86346°
Mean anomaly
228.6781°
Eccentric anomaly
225.73638°
Mean motion
3.34802 °/min
Orbital period
107.53 mins
BSTAR
0.000083918
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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 DEB 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-10 09:01:10.342Z | 190.345° SSW | 2026-05-10 09:04:10.342Z | 165.297° S | 17.832° | 2026-05-10 09:09:10.342Z | 118.521° SE |
| 9 mins | 2026-05-10 10:54:10.342Z | 222.535° SW | 2026-05-10 10:58:10.342Z | 178.93° S | 26.561° | 2026-05-10 11:03:10.342Z | 114.689° SE |
| 8 mins | 2026-05-10 12:48:10.342Z | 239.731° WSW | 2026-05-10 12:52:10.342Z | 185.572° SSW | 26.121° | 2026-05-10 12:56:10.342Z | 128.477° SE |
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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