DELTA 1 R/B, 1983

Orbit data source: Space-Track

DELTA 1 R/B, 1983 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
1983, 1966-008B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
60 kg wet, 60 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
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 DELTA 1 R/B
1 01983U 66008B   25259.47920378  .00001045  00000-0  18686-3 0  9996
2 01983  98.0260 176.9266 0063209 243.2249 116.2480 14.67745224132472
Epoch: 2025-09-16T11:30Z
TLE epoch observation values (Epoch: 2025-09-16T11:30:03.206Z)
Latitude
-0.00006°
Longitude
8.74433°
Altitude
691.204 km
Speed
7.5 km/s
True Right ascension
11h 47m 42s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
01:08:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
709.859 km
Perigee altitude
620.817 km
Semi-major axis
7,043.475 km
Eccentricity
0.00632
Inclination
98.026°
RAAN
176.9266°
Arg. of periapsis
243.2249°
True anomaly
116.89536°
Mean anomaly
116.248°
Eccentric anomaly
116.57191°
Mean motion
3.67166 °/min
Orbital period
98.05 mins
BSTAR
0.00018686
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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

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