DELTA 1 DEB, 2154

Orbit data source: Space-Track

DELTA 1 DEB, 2154 is space debris in SSO originally from a launch on Thu, 03 Feb 1966 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
2154, 1966-008E
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1966-02-03 (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: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 02154U 66008E   25305.30245566  .00001830  00000-0  30117-3 0  9995
2 02154  97.8545  64.1983 0045932 319.2585  40.5190 14.71045639145503
Epoch: 2025-11-01T07:15Z
TLE epoch observation values (Epoch: 2025-11-01T07:15:32.169Z)
Latitude
Longitude
-85.52022°
Altitude
636.233 km
Speed
7.553 km/s
True Right ascension
04h 16m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
08:26:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
687.086 km
Perigee altitude
622.479 km
Semi-major axis
7,032.92 km
Eccentricity
0.00459
Inclination
97.8545°
RAAN
64.1983°
Arg. of periapsis
319.2585°
True anomaly
40.86246°
Mean anomaly
40.519°
Eccentric anomaly
40.69058°
Mean motion
3.67993 °/min
Orbital period
97.83 mins
BSTAR
0.00030117
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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