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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 02888U 65089D   25260.38560479 -.00000044  00000-0  21976-3 0  9998
2 02888  59.1973 238.0985 0722100  71.8898   6.2316 11.87419678542090
Epoch: 2025-09-17T09:15Z
TLE epoch observation values (Epoch: 2025-09-17T09:15:16.253Z)
Latitude
57.63792°
Longitude
172.10174°
Altitude
1,163.884 km
Speed
7.534 km/s
True Right ascension
20h 29m 55s
True Declination
57° 29' 26"
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
09:50:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,323.105 km
Perigee altitude
1,151.102 km
Semi-major axis
8,115.241 km
Eccentricity
0.07221
Inclination
59.1973°
RAAN
238.0985°
Arg. of periapsis
71.8898°
True anomaly
7.21789°
Mean anomaly
6.2316°
Eccentric anomaly
6.71541°
Mean motion
2.96887 °/min
Orbital period
121.26 mins
BSTAR
0.00021976
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