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
2))"
Bus & Motor
DCSS-4, RL10B-2
Mass
2,850 kg wet, 2,850 kg dry
Launch date (UTC)
2006-05-24 (19 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: 2 days ago

TLE from 2 days ago
0 DELTA 4 R/B
1 29156U 06018B   25240.91805519 -.00000224  00000-0  00000-0 0  9998
2 29156  13.1193 301.7404 5254381 328.3443 243.4349  1.93077727135828
Epoch: 2025-08-28T22:01Z
TLE epoch observation values (Epoch: 2025-08-28T22:01:59.968Z)
Latitude
1.55987°
Longitude
167.19878°
Altitude
31,342.459 km
Speed
2.55 km/s
True Right ascension
07h 40m 17s
True Declination
1° 33' 29"
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
09:12:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,182.34 km
Perigee altitude
6,551.276 km
Semi-major axis
27,244.945 km
Eccentricity
0.52544
Inclination
13.1193°
RAAN
301.7404°
Arg. of periapsis
328.3443°
True anomaly
204.73994°
Mean anomaly
243.4349°
Eccentric anomaly
222.92999°
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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