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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 DELTA 1 DEB
1 02154U 66008E   25260.88264169  .00001316  00000-0  21935-3 0  9995
2 02154  97.8486  21.3832 0048304 100.2667 260.3992 14.70834966138973
Epoch: 2025-09-17T21:11Z
TLE epoch observation values (Epoch: 2025-09-17T21:11:00.242Z)
Latitude
0.00004°
Longitude
66.57998°
Altitude
667.244 km
Speed
7.52 km/s
True Right ascension
01h 25m 31s
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
01:44:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.43 km
Perigee altitude
621.479 km
Semi-major axis
7,033.592 km
Eccentricity
0.00483
Inclination
97.8486°
RAAN
21.3832°
Arg. of periapsis
100.2667°
True anomaly
259.85399°
Mean anomaly
260.3992°
Eccentric anomaly
260.12654°
Mean motion
3.6794 °/min
Orbital period
97.84 mins
BSTAR
0.00021935
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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