ATLAS CENTAUR R/B, 10722
Orbit data source: Space-Track
ATLAS CENTAUR R/B, 10722 is space debris in HEO originally from a launch on Sat, 07 Jan 1978 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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10722 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
CENTAUR, Unknown motor
Mass
~1,800 kg wet, ~1,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ATLAS CENTAUR R/B
1 10722U 78002B 26124.14236062 -.00000088 00000-0 59270-3 0 9991
2 10722 21.8901 354.9593 7164685 147.4739 5.1129 2.21864723283630Epoch: 2026-05-04T03:24Z
TLE epoch observation values (Epoch: 2026-05-04T03:24:59.957Z)
Latitude
-3.04356°
Longitude
-90.76416°
Altitude
1,480.41 km
Speed
9.24 km/s
True Right ascension
12h 10m 05s
True Declination
-3° 01' 37"
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
22:41:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,252.134 km
Perigee altitude
663.661 km
Semi-major axis
24,836.035 km
Eccentricity
0.71647
Inclination
21.8901°
RAAN
354.9593°
Arg. of periapsis
147.4739°
True anomaly
41.18438°
Mean anomaly
5.1129°
Eccentric anomaly
17.3643°
Mean motion
0.55452 °/min
Orbital period
649.21 mins
BSTAR
0.0005927
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Other satellites on launch #2 in the year 1978 (1978-01-07 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 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. |
|---|---|---|---|---|---|---|---|
| 181 mins | 2026-05-05 14:47:35.044Z | 217.595° SW | 2026-05-05 15:24:35.044Z | 221.331° SW | 14.402° | 2026-05-05 17:48:35.044Z | 239.366° WSW |
| 43 mins | 2026-05-05 21:40:35.044Z | 258.365° W | 2026-05-05 22:17:35.044Z | 206.243° SW | 28.902° | 2026-05-05 22:23:35.044Z | 148.983° SSE |
| 259 mins | 2026-05-06 10:28:35.044Z | 187.093° SSW | 2026-05-06 14:47:35.044Z | 199.869° SSW | 26.196° | 2026-05-06 14:47:35.044Z | 199.869° SSW |
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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