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 (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: 2 weeks ago

TLE from 2 weeks ago
0 DELTA 1 DEB
1 28662U 65089G   26083.97828580 -.00000223  00000-0 -52409-3 0  9990
2 28662  59.3878 164.0867 0736332  94.3802  77.5189 12.24892809971513
Epoch: 2026-03-24T23:28Z
TLE epoch observation values (Epoch: 2026-03-24T23:28:43.893Z)
Latitude
-0.31883°
Longitude
169.64335°
Altitude
1,488.112 km
Speed
7.158 km/s
True Right ascension
22h 57m 05s
True Declination
0° 19' 02"
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
21:19:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,155.983 km
Perigee altitude
985.389 km
Semi-major axis
7,948.823 km
Eccentricity
0.07363
Inclination
59.3878°
RAAN
164.0867°
Arg. of periapsis
94.3802°
True anomaly
85.8943°
Mean anomaly
77.5189°
Eccentric anomaly
81.69351°
Mean motion
3.06259 °/min
Orbital period
117.55 mins
BSTAR
-0.00052409
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