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
2))"
Bus & Motor
DCSS-4, RL10B-2
Mass
2,850 kg wet, 2,850 kg dry
Launch date (UTC)
2015-03-25 (10 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, Unknown HBR
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   25240.71191706  .00000050  00000-0  00000-0 0  9997
2 40535  52.7293 227.4002 0032799  62.3549 297.9653  1.92974721 73512
Epoch: 2025-08-28T17:05Z
TLE epoch observation values (Epoch: 2025-08-28T17:05:09.633Z)
Latitude
-0.00003°
Longitude
-6.06483°
Altitude
20,832.607 km
Speed
3.83 km/s
True Right ascension
15h 09m 35s
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
03:09:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,963.545 km
Perigee altitude
20,784.775 km
Semi-major axis
27,252.297 km
Eccentricity
0.00328
Inclination
52.7293°
RAAN
227.4002°
Arg. of periapsis
62.3549°
True anomaly
297.6327°
Mean anomaly
297.9653°
Eccentric anomaly
297.79906°
Mean motion
0.48243 °/min
Orbital period
746.22 mins
BSTAR
0
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