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   25258.53829954 -.00000043  00000-0  22654-3 0  9991
2 02888  59.1972 242.1963 0722084  70.6575  29.5291 11.87419576541873
Epoch: 2025-09-15T12:55Z
TLE epoch observation values (Epoch: 2025-09-15T12:55:09.08Z)
Latitude
56.34795°
Longitude
170.66769°
Altitude
1,247.041 km
Speed
7.457 km/s
True Right ascension
23h 56m 47s
True Declination
56° 11' 58"
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
10:16:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,323.093 km
Perigee altitude
1,151.115 km
Semi-major axis
8,115.241 km
Eccentricity
0.07221
Inclination
59.1972°
RAAN
242.1963°
Arg. of periapsis
70.6575°
True anomaly
33.94914°
Mean anomaly
29.5291°
Eccentric anomaly
31.7033°
Mean motion
2.96887 °/min
Orbital period
121.26 mins
BSTAR
0.00022654
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