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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago
0 DELTA 1 DEB
1 02888U 65089D   26042.15572982 -.00000048  00000-0  17477-3 0  9999
2 02888  59.1995 272.5634 0719281 169.9219 288.6059 11.87424678559522
Epoch: 2026-02-11T03:44Z
TLE epoch observation values (Epoch: 2026-02-11T03:44:15.056Z)
Latitude
59.31808°
Longitude
166.27351°
Altitude
1,598.99 km
Speed
7.14 km/s
True Right ascension
00h 14m 14s
True Declination
59° 10' 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
08:09:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,320.793 km
Perigee altitude
1,153.368 km
Semi-major axis
8,115.218 km
Eccentricity
0.07193
Inclination
59.1995°
RAAN
272.5634°
Arg. of periapsis
169.9219°
True anomaly
280.59022°
Mean anomaly
288.6059°
Eccentric anomaly
284.61813°
Mean motion
2.96888 °/min
Orbital period
121.26 mins
BSTAR
0.00017477
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