DELTA 4 R/B, 39742

Orbit data source: Space-Track

DELTA 4 R/B, 39742 is space debris in MEO originally from a launch on Sat, 17 May 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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Identifier
39742, 2014-026B
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)
2014-05-17 (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: 4 days ago

TLE from 4 days ago
0 DELTA 4 R/B
1 39742U 14026B   25304.84864356 -.00000063  00000-0  00000-0 0  9996
2 39742  56.6971 351.2141 0013349 129.8191 230.3623  1.93898843 78646
Epoch: 2025-10-31T20:22Z
TLE epoch observation values (Epoch: 2025-10-31T20:22:02.803Z)
Latitude
0.00002°
Longitude
5.33087°
Altitude
20,810.873 km
Speed
3.827 km/s
True Right ascension
23h 24m 55s
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
23:25:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,823.607 km
Perigee altitude
20,751.08 km
Semi-major axis
27,165.48 km
Eccentricity
0.00133
Inclination
56.6971°
RAAN
351.2141°
Arg. of periapsis
129.8191°
True anomaly
230.24463°
Mean anomaly
230.3623°
Eccentric anomaly
230.30345°
Mean motion
0.48475 °/min
Orbital period
742.65 mins
BSTAR
0
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