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: 6 days ago

TLE from 6 days ago
0 DELTA 1 DEB
1 02888U 65089D   26273.85954896 -.00000069  00000-0  24838-4 0  9993
2 02888  59.2001 118.7598 0715883 326.2116  42.4850 11.87432366587045
Epoch: 2026-09-30T20:37Z
TLE epoch observation values (Epoch: 2026-09-30T20:37:45.030Z)
Latitude
12.50957°
Longitude
167.27976°
Altitude
1,330.278 km
Speed
7.372 km/s
True Right ascension
08h 25m 17s
True Declination
12° 26' 33"
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
12:28:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,317.998 km
Perigee altitude
1,156.093 km
Semi-major axis
8,115.182 km
Eccentricity
0.07159
Inclination
59.2001°
RAAN
118.7598°
Arg. of periapsis
326.2116°
True anomaly
48.40519°
Mean anomaly
42.485°
Eccentric anomaly
45.40581°
Mean motion
2.9689 °/min
Orbital period
121.26 mins
BSTAR
0.000024838
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