ATLAS CENTAUR 2 DEB, 701
Orbit data source: Space-Track
ATLAS CENTAUR 2 DEB, 701 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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701 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G 25286.86211390 .00001500 00000-0 47632-3 0 9992
2 00701 30.0126 337.9639 0506802 349.7025 9.3505 13.82674154 76098
Epoch: 2025-10-13T20:41Z
TLE epoch observation values (Epoch: 2025-10-13T20:41:26.640Z)
Latitude
-0.00005°
Longitude
4.944°
Altitude
586.87 km
Speed
7.755 km/s
True Right ascension
22h 31m 51s
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
01:35:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,329.996 km
Perigee altitude
586.383 km
Semi-major axis
7,336.327 km
Eccentricity
0.05068
Inclination
30.0126°
RAAN
337.9639°
Arg. of periapsis
349.7025°
True anomaly
10.35675°
Mean anomaly
9.3505°
Eccentric anomaly
9.8471°
Mean motion
3.45402 °/min
Orbital period
104.23 mins
BSTAR
0.00047632
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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. |
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6 mins | 2025-10-14 07:19:27.398Z | 190.285° SSW | 2025-10-14 07:22:27.398Z | 152.028° SSE | 16.976° | 2025-10-14 07:25:27.398Z | 119.889° SE |
9 mins | 2025-10-14 09:08:27.398Z | 222.56° SW | 2025-10-14 09:11:27.398Z | 180.854° SSW | 27.873° | 2025-10-14 09:17:27.398Z | 113.699° SE |
10 mins | 2025-10-14 10:58:27.398Z | 236.44° WSW | 2025-10-14 11:02:27.398Z | 183.612° SSW | 28.522° | 2025-10-14 11:08:27.398Z | 128.776° SE |
8 mins | 2025-10-14 12:49:27.398Z | 231.917° WSW | 2025-10-14 12:52:27.398Z | 202.874° SW | 19.721° | 2025-10-14 12:57:27.398Z | 161.047° S |
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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