View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 33879U 97051AY 23064.91356809 .10900305 25741+0 38216-1 0 9995
2 33879 86.3032 19.5990 0023543 177.8372 182.3019 15.95577958498173
Epoch (UTC): | 05 March 2023 21:55:32 |
Eccentricity: | 0.0023543 |
inclination: | 86.3032° |
perigee height: | 271 km |
apogee height: | 302 km |
right ascension of ascending node: | 19.5990° |
argument of perigee: | 177.8372° |
revolutions per day: | 15.95577958 |
mean anomaly at epoch: | 182.3019° |
orbit number at epoch: | 49817 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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