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, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 DELTA 1 DEB
1 02888U 65089D   26208.55277307 -.00000008  00000-0  44986-3 0  9991
2 02888  59.2045 263.5750 0714895 282.1338 232.1586 11.87432189579284
Epoch: 2026-07-27T13:15Z
TLE epoch observation values (Epoch: 2026-07-27T13:15:59.593Z)
Latitude
26.99054°
Longitude
-78.24704°
Altitude
2,119.503 km
Speed
6.69 km/s
True Right ascension
04h 23m 56s
True Declination
26° 52' 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
15:13:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,317.196 km
Perigee altitude
1,156.895 km
Semi-major axis
8,115.183 km
Eccentricity
0.07149
Inclination
59.2045°
RAAN
263.575°
Arg. of periapsis
282.1338°
True anomaly
226.03766°
Mean anomaly
232.1586°
Eccentric anomaly
229.06426°
Mean motion
2.9689 °/min
Orbital period
121.26 mins
BSTAR
0.00044986
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