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  2154U 66008E   26144.03364499  .00000705  00000-0  11899-3 0  9990
2  2154  97.8715 260.9745 0046764  26.9578 333.4044 14.71757799175469
Epoch: 2026-05-24T00:48Z
TLE epoch observation values (Epoch: 2026-05-24T00:48:26.927Z)
Latitude
-0.00002°
Longitude
7.22071°
Altitude
629.086 km
Speed
7.56 km/s
True Right ascension
17h 23m 53s
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
12:26:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
685.391 km
Perigee altitude
619.634 km
Semi-major axis
7,030.65 km
Eccentricity
0.00468
Inclination
97.8715°
RAAN
260.9745°
Arg. of periapsis
26.9578°
True anomaly
333.16323°
Mean anomaly
333.4044°
Eccentric anomaly
333.28394°
Mean motion
3.68171 °/min
Orbital period
97.78 mins
BSTAR
0.00011899
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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