DELTA 1 DEB, 28662

Orbit data source: Space-Track

DELTA 1 DEB, 28662 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
28662, 1965-089G
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-11-06 (61 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: 6 days ago

TLE from 6 days ago
0 DELTA 1 DEB
1 28662U 65089G   26144.38288610  .00001970  00000-0  77237-2 0  9990
2 28662  59.3966  20.8314 0734615 135.2382  38.1179 12.24972551978913
Epoch: 2026-05-24T09:11Z
TLE epoch observation values (Epoch: 2026-05-24T09:11:21.359Z)
Latitude
0.82943°
Longitude
-179.48152°
Altitude
1,130.583 km
Speed
7.488 km/s
True Right ascension
13h 21m 22s
True Declination
0° 49' 29"
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
21:52:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,154.247 km
Perigee altitude
986.433 km
Semi-major axis
7,948.477 km
Eccentricity
0.07346
Inclination
59.3966°
RAAN
20.8314°
Arg. of periapsis
135.2382°
True anomaly
43.70851°
Mean anomaly
38.1179°
Eccentric anomaly
40.87218°
Mean motion
3.06279 °/min
Orbital period
117.54 mins
BSTAR
0.0077237
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