ATLAS CENTAUR 2 DEB, 2886
Orbit data source: Space-Track
ATLAS CENTAUR 2 DEB, 2886 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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2886 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ATLAS CENTAUR 2 DEB
1 02886U 63047K 26104.16001456 .00000109 00000-0 36589-4 0 9995
2 02886 29.8687 141.3009 0643307 101.1437 266.2102 13.29977039867688Epoch: 2026-04-14T03:50Z
TLE epoch observation values (Epoch: 2026-04-14T03:50:25.257Z)
Latitude
-0.00005°
Longitude
-118.64467°
Altitude
1,208.08 km
Speed
7.222 km/s
True Right ascension
09h 25m 12s
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
21:13:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,634.88 km
Perigee altitude
666.228 km
Semi-major axis
7,528.691 km
Eccentricity
0.06433
Inclination
29.8687°
RAAN
141.3009°
Arg. of periapsis
101.1437°
True anomaly
258.91322°
Mean anomaly
266.2102°
Eccentric anomaly
262.55539°
Mean motion
3.32249 °/min
Orbital period
108.35 mins
BSTAR
0.000036589
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-15 05:16:34.803Z | 185.481° SSW | 2026-04-15 05:18:34.803Z | 165.849° S | 13.131° | 2026-04-15 05:21:34.803Z | 133.136° SE |
| 6 mins | 2026-04-15 07:10:34.803Z | 212.472° SW | 2026-04-15 07:13:34.803Z | 168.556° S | 21.718° | 2026-04-15 07:16:34.803Z | 125.535° SE |
| 5 mins | 2026-04-15 09:05:34.803Z | 220.096° SW | 2026-04-15 09:07:34.803Z | 185.262° SSW | 21.98° | 2026-04-15 09:10:34.803Z | 138.873° 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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