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
Last TLE update
9 hours ago
Origin
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
1966-02-03 (59 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

TLE from 9 hours ago
0 DELTA 1 R/B
1  1983U 66008B   25200.23370085  .00000954  00000-0  17128-3 0  9998
2  1983  98.0298 118.8430 0066299  71.9061 288.9351 14.67563151144677
Epoch: 2025-07-19T05:36Z
TLE epoch observation values (Epoch: 2025-07-19T05:36:31.753Z)
Latitude
0.00001°
Longitude
97.43695°
Altitude
656.973 km
Speed
7.537 km/s
True Right ascension
07h 55m 22s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-6.29604°
Longitude
-83.0816°
Altitude
692.744 km
Speed
7.499 km/s
Apparent Right ascension
18h 07m 14s
Apparent Declination
-25° 43' 14"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
03:27:54
Azimuth
280.894° WNW
Elevation
-54.008°
Doppler factor
1
Orbital elements
Apogee altitude
712.623 km
Perigee altitude
619.22 km
Semi-major axis
7,044.058 km
Eccentricity
0.00663
Inclination
98.0298°
RAAN
118.843°
Arg. of periapsis
71.9061°
True anomaly
288.21456°
Mean anomaly
288.9351°
Eccentric anomaly
288.57502°
Mean motion
3.67121 °/min
Orbital period
98.06 mins
BSTAR
0.00017128
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