DELTA 4 R/B, 29156

Orbit data source: Space-Track

DELTA 4 R/B, 29156 is space debris in HEO originally from a launch on Wed, 24 May 2006 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
29156, 2006-018B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
ULA Decatur
Mission
Spacecraft
Bus & Motor
DCSS-4, RL10B-2
Mass
2,850 kg wet, 2,850 kg dry
Launch date (UTC)
2006-05-24 (20 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: 16 hours ago

TLE from 16 hours ago
0 DELTA 4 R/B
1 29156U 06018B   26094.88051322 -.00000131  00000-0  00000-0 0  9994
2 29156  12.4403 276.5923 5264266  17.1276 158.9426  1.93078644140055
Epoch: 2026-04-04T21:07Z
TLE epoch observation values (Epoch: 2026-04-04T21:07:56.342Z)
Latitude
-2.03043°
Longitude
-44.40444°
Altitude
34,756.95 km
Speed
2.179 km/s
True Right ascension
07h 03m 05s
True Declination
-2° 01' 42"
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
19:30:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,209.179 km
Perigee altitude
6,524.315 km
Semi-major axis
27,244.884 km
Eccentricity
0.52643
Inclination
12.4403°
RAAN
276.5923°
Arg. of periapsis
17.1276°
True anomaly
172.26432°
Mean anomaly
158.9426°
Eccentric anomaly
166.15848°
Mean motion
0.48263 °/min
Orbital period
745.91 mins
BSTAR
0
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Other satellites on launch #18 in the year 2006 (2006-05-24 UTC)

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