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: 2 weeks ago

TLE from 2 weeks ago
0 DELTA 1 DEB
1 02888U 65089D   26148.09570259 -.00000073  00000-0 -82806-5 0  9993
2 02888  59.2064  37.6274 0715572 241.3076 273.8481 11.87428175572105
Epoch: 2026-05-28T02:17Z
TLE epoch observation values (Epoch: 2026-05-28T02:17:48.703Z)
Latitude
27.99499°
Longitude
-80.85033°
Altitude
1,742.09 km
Speed
7.009 km/s
True Right ascension
13h 16m 59s
True Declination
27° 52' 12"
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
12:56:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,317.765 km
Perigee altitude
1,156.363 km
Semi-major axis
8,115.201 km
Eccentricity
0.07156
Inclination
59.2064°
RAAN
37.6274°
Arg. of periapsis
241.3076°
True anomaly
265.64547°
Mean anomaly
273.8481°
Eccentric anomaly
269.74821°
Mean motion
2.96889 °/min
Orbital period
121.26 mins
BSTAR
-0.0000082806
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