Satellite description
DELTA 1 DEB (YO), 167 is space debris in LEO originally from a launch on Wed, 12 Jul 1961 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.
Satellite metadata
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Sunlit
Orbital elements
Apogee altitude
877.49 km
Perigee altitude
747.884 km
Semi-major axis
7,190.824 km
Eccentricity
0.00901
Inclination
47.8431°
RAAN
166.5485°
Arg. of periapsis
50.8128°
True anomaly
309.2757°
Mean anomaly
310.0717°
Eccentric anomaly
309.67428°
Mean motion
3.55939 °/min
Orbital period
101.14 mins
BSTAR
0.00028697