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: 3 days ago

TLE from 3 days ago
0 DELTA 1 DEB
1 02888U 65089D   25317.98534931 -.00000028  00000-0  32886-3 0  9995
2 02888  59.1970 110.3359 0722360 110.3009 349.3706 11.87425382548937
Epoch: 2025-11-13T23:38Z
TLE epoch observation values (Epoch: 2025-11-13T23:38:54.180Z)
Latitude
58.40518°
Longitude
167.63171°
Altitude
1,171.471 km
Speed
7.527 km/s
True Right ascension
14h 22m 46s
True Declination
58° 15' 36"
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
18:09:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,323.288 km
Perigee altitude
1,150.867 km
Semi-major axis
8,115.215 km
Eccentricity
0.07224
Inclination
59.197°
RAAN
110.3359°
Arg. of periapsis
110.3009°
True anomaly
347.69594°
Mean anomaly
349.3706°
Eccentric anomaly
348.54892°
Mean motion
2.96888 °/min
Orbital period
121.26 mins
BSTAR
0.00032886
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