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 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.064 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 DELTA 1 DEB
1  2888U 65089D   26314.64618727 -.00000038  00000-0  24537-3 0  9997
2  2888  59.2046  28.3096 0717444 353.6253 155.3660 11.87432995591882
Epoch: 2026-11-10T15:30Z
TLE epoch observation values (Epoch: 2026-11-10T15:30:30.580Z)
Latitude
23.69037°
Longitude
-89.21418°
Altitude
2,274.812 km
Speed
6.563 km/s
True Right ascension
12h 52m 52s
True Declination
23° 35' 10"
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
02:14:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,319.261 km
Perigee altitude
1,154.823 km
Semi-major axis
8,115.179 km
Eccentricity
0.07174
Inclination
59.2046°
RAAN
28.3096°
Arg. of periapsis
353.6253°
True anomaly
158.53223°
Mean anomaly
155.366°
Eccentric anomaly
156.97388°
Mean motion
2.9689 °/min
Orbital period
121.26 mins
BSTAR
0.00024537
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