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: 11 hours ago

TLE from 11 hours ago
0 DELTA 1 DEB
1  2154U 66008E   26091.27376594  .00001712  00000-0  27842-3 0  9990
2  2154  97.8631 209.9539 0046191 192.6845 167.3204 14.71634663167706
Epoch: 2026-04-01T06:34Z
TLE epoch observation values (Epoch: 2026-04-01T06:34:13.377Z)
Latitude
-0.00001°
Longitude
-78.24079°
Altitude
690.578 km
Speed
7.494 km/s
True Right ascension
13h 59m 48s
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
23:14:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
685.382 km
Perigee altitude
620.428 km
Semi-major axis
7,031.042 km
Eccentricity
0.00462
Inclination
97.8631°
RAAN
209.9539°
Arg. of periapsis
192.6845°
True anomaly
167.43593°
Mean anomaly
167.3204°
Eccentric anomaly
167.37823°
Mean motion
3.68141 °/min
Orbital period
97.79 mins
BSTAR
0.00027842
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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