Satellite description
THOR DELTA 1 R/B, 5106 is space debris in LEO originally from a launch on Thu, 01 Apr 1971 UTC launched from the Air Force Western Test Range (AFWTR). 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.
Satellite metadata
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Sunlit
Orbital elements
Apogee altitude
1,418.412 km
Perigee altitude
1,348.696 km
Semi-major axis
7,761.691 km
Eccentricity
0.00449
Inclination
88.1638°
RAAN
319.6044°
Arg. of periapsis
132.9155°
True anomaly
40.67265°
Mean anomaly
40.3381°
Eccentric anomaly
40.50523°
Mean motion
3.17401 °/min
Orbital period
113.42 mins
BSTAR
0.000066133