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 (12 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: 14 hours ago

TLE from 14 hours ago
0 DELTA 4 R/B
1 39742U 14026B   26048.15022491 -.00000080  00000-0  00000+0 0  9990
2 39742  56.6784 347.3118 0012870 126.5400 233.5858  1.93898921 80749
Epoch: 2026-02-17T03:36Z
TLE epoch observation values (Epoch: 2026-02-17T03:36:19.432Z)
Latitude
0.00003°
Longitude
146.08384°
Altitude
20,808.589 km
Speed
3.828 km/s
True Right ascension
23h 09m 11s
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
20:05:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,822.299 km
Perigee altitude
20,752.375 km
Semi-major axis
27,165.474 km
Eccentricity
0.00129
Inclination
56.6784°
RAAN
347.3118°
Arg. of periapsis
126.54°
True anomaly
233.46723°
Mean anomaly
233.5858°
Eccentric anomaly
233.5265°
Mean motion
0.48475 °/min
Orbital period
742.65 mins
BSTAR
0
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