ATLAS 5 CENTAUR R/B, 40295
Orbit data source: Space-Track
ATLAS 5 CENTAUR R/B, 40295 is space debris in MEO originally from a launch on Wed, 29 Oct 2014 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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40295 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10-4A-2
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 5.8 m
Radar Cross Section
32.260 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 ATLAS 5 CENTAUR R/B
1 40295U 14068B 25347.93858093 -.00000093 00000-0 00000-0 0 9998
2 40295 57.1057 53.3427 0119816 350.4378 9.3776 1.91825467 77961Epoch: 2025-12-13T22:31Z
TLE epoch observation values (Epoch: 2025-12-13T22:31:33.392Z)
Latitude
-0.00002°
Longitude
-7.39189°
Altitude
20,659.643 km
Speed
3.862 km/s
True Right ascension
03h 33m 25s
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
18:25:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,310.553 km
Perigee altitude
20,654.899 km
Semi-major axis
27,360.863 km
Eccentricity
0.01198
Inclination
57.1057°
RAAN
53.3427°
Arg. of periapsis
350.4378°
True anomaly
9.60467°
Mean anomaly
9.3776°
Eccentric anomaly
9.4908°
Mean motion
0.47957 °/min
Orbital period
750.68 mins
BSTAR
0
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Other satellites on launch #68 in the year 2014 (2014-10-29 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 5 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. |
|---|---|---|---|---|---|---|---|
| 69 mins | 2025-12-15 00:55:08.025Z | 65.956° ENE | 2025-12-15 01:30:08.025Z | 51.674° ENE | 12.17° | 2025-12-15 02:04:08.025Z | 38.541° NE |
| 318 mins | 2025-12-15 14:03:08.025Z | 310.368° NW | 2025-12-15 16:45:08.025Z | 266.96° W | 41.898° | 2025-12-15 19:21:08.025Z | 199.9° 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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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 descending order |
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