DELTA 2 DEB, 29534

Orbit data source: Space-Track

DELTA 2 DEB, 29534 is space debris in HEO originally from a launch on Mon, 26 Sep 2005 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
29534, 2005-038D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Boeing/HB
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Wet unknown, 1 kg dry
Launch date (UTC)
2005-09-26 (21 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Cable, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago
0 DELTA 2 DEB
1 29534U 05038D   26160.54106698  .00008778  00000-0  88038-3 0  9993
2 29534  39.4820 335.9415 5738934 110.3318 318.0499  4.47243033309351
Epoch: 2026-06-09T12:59Z
TLE epoch observation values (Epoch: 2026-06-09T12:59:08.187Z)
Latitude
-0.00007°
Longitude
-116.76091°
Altitude
6,637.841 km
Speed
5.97 km/s
True Right ascension
22h 23m 44s
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
03:44:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
18,116.536 km
Perigee altitude
253.406 km
Semi-major axis
15,563.108 km
Eccentricity
0.57389
Inclination
39.482°
RAAN
335.9415°
Arg. of periapsis
110.3318°
True anomaly
249.76323°
Mean anomaly
318.0499°
Eccentric anomaly
286.52665°
Mean motion
1.11789 °/min
Orbital period
322.04 mins
BSTAR
0.00088038
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Other satellites on launch #38 in the year 2005 (2005-09-26 UTC)

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