DELTA 1 DEB, 2888

Orbit data source: Space-Track

DELTA 1 DEB, 2888 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
2888, 1965-089D
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 days ago

TLE from 2 days ago
0 DELTA 1 DEB
1 02888U 65089D   25304.67537660 -.00000036  00000-0  27108-3 0  9999
2 02888  59.1964 139.8612 0722494 101.4118 332.7887 11.87424642547357
Epoch: 2025-10-31T16:12Z
TLE epoch observation values (Epoch: 2025-10-31T16:12:32.538Z)
Latitude
53.98846°
Longitude
-88.79762°
Altitude
1,233.37 km
Speed
7.469 km/s
True Right ascension
12h 58m 13s
True Declination
53° 50' 06"
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
14:22:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,323.401 km
Perigee altitude
1,150.761 km
Semi-major axis
8,115.218 km
Eccentricity
0.07225
Inclination
59.1964°
RAAN
139.8612°
Arg. of periapsis
101.4118°
True anomaly
328.67708°
Mean anomaly
332.7887°
Eccentric anomaly
330.76709°
Mean motion
2.96888 °/min
Orbital period
121.26 mins
BSTAR
0.00027108
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