DELTA 1 DEB, 2118

Orbit data source: Space-Track

DELTA 1 DEB, 2118 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
2118, 1966-008D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
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: 9 hours ago

TLE from 9 hours ago
0 DELTA 1 DEB
1 02118U 66008D   25288.88653791  .00001484  00000-0  38620-3 0  9993
2 02118  98.0270  68.2449 0125588 251.9202 106.8278 14.46426207100507
Epoch: 2025-10-15T21:16Z
TLE epoch observation values (Epoch: 2025-10-15T21:16:36.875Z)
Latitude
0.00005°
Longitude
84.43707°
Altitude
767.215 km
Speed
7.456 km/s
True Right ascension
04h 32m 58s
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
00:40:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
823.761 km
Perigee altitude
645.11 km
Semi-major axis
7,112.573 km
Eccentricity
0.01256
Inclination
98.027°
RAAN
68.2449°
Arg. of periapsis
251.9202°
True anomaly
108.19894°
Mean anomaly
106.8278°
Eccentric anomaly
107.51401°
Mean motion
3.61829 °/min
Orbital period
99.49 mins
BSTAR
0.0003862
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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