DELTA 4 R/B, 40535

Orbit data source: Space-Track

DELTA 4 R/B, 40535 is space debris in MEO originally from a launch on Wed, 25 Mar 2015 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
40535, 2015-013B
Orbit
MEO
Country
Flag of USUS
Related business
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
ULA Decatur
Mission
Spacecraft
Bus & Motor
DCSS-4, RL10B-2
Mass
2,850 kg wet, 2,850 kg dry
Launch date (UTC)
2015-03-25 (11 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.0 m
Radar Cross Section
43.982 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 DELTA 4 R/B
1 40535U 15013B   25340.20306810  .00000042  00000-0  00000-0 0  9997
2 40535  52.6935 223.5717 0034310  64.0955 296.3510  1.92974475 75439
Epoch: 2025-12-06T04:52Z
TLE epoch observation values (Epoch: 2025-12-06T04:52:25.083Z)
Latitude
0.00007°
Longitude
75.24317°
Altitude
20,833.075 km
Speed
3.83 km/s
True Right ascension
14h 54m 19s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:21:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,967.688 km
Perigee altitude
20,780.682 km
Semi-major axis
27,252.322 km
Eccentricity
0.00343
Inclination
52.6935°
RAAN
223.5717°
Arg. of periapsis
64.0955°
True anomaly
295.99802°
Mean anomaly
296.351°
Eccentric anomaly
296.17458°
Mean motion
0.48243 °/min
Orbital period
746.22 mins
BSTAR
0
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