DELTA 1 DEB, 29010

Orbit data source: Space-Track

DELTA 1 DEB, 29010 is space debris in LEO originally from a launch on Sat, 06 Nov 1965 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
29010, 1965-089H
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-11-06 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 DELTA 1 DEB
1 29010U 65089H   26125.49005478 -.00000081  00000-0 -16972-4 0  9993
2 29010  59.2696 187.7770 0657408 153.0421 241.6056 12.09405358519820
Epoch: 2026-05-05T11:45Z
TLE epoch observation values (Epoch: 2026-05-05T11:45:40.732Z)
Latitude
24.07719°
Longitude
163.32483°
Altitude
1,916.6 km
Speed
6.815 km/s
True Right ascension
13h 32m 26s
True Declination
23° 58' 02"
Sunlit
Object was in full shadow 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
03:10:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,165.445 km
Perigee altitude
1,111.414 km
Semi-major axis
8,016.567 km
Eccentricity
0.06574
Inclination
59.2696°
RAAN
187.777°
Arg. of periapsis
153.0421°
True anomaly
235.24119°
Mean anomaly
241.6056°
Eccentric anomaly
238.39751°
Mean motion
3.02385 °/min
Orbital period
119.05 mins
BSTAR
-0.000016972
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