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: 21 hours ago

TLE from 21 hours ago
0 DELTA 1 DEB
1 02154U 66008E   25242.10597598  .00002171  00000-0  35763-3 0  9999
2 02154  97.8463   3.3004 0047624 159.0468 201.2705 14.70758488136219
Epoch: 2025-08-30T02:32Z
TLE epoch observation values (Epoch: 2025-08-30T02:32:36.324Z)
Latitude
-0.00001°
Longitude
-13.39599°
Altitude
692.915 km
Speed
7.493 km/s
True Right ascension
00h 13m 12s
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
15:37:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.196 km
Perigee altitude
622.201 km
Semi-major axis
7,033.835 km
Eccentricity
0.00476
Inclination
97.8463°
RAAN
3.3004°
Arg. of periapsis
159.0468°
True anomaly
201.07362°
Mean anomaly
201.2705°
Eccentric anomaly
201.17195°
Mean motion
3.67921 °/min
Orbital period
97.85 mins
BSTAR
0.00035763
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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