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 20478U 90013A 21063.94452858 .00000217 00000-0 19391-3 0 9997
2 20478 99.4308 71.7071 0005958 33.0838 327.0695 13.95523942502766
Epoch (UTC): | 04 March 2021 22:40:07 |
Eccentricity: | 0.0005958 |
inclination: | 99.4308° |
perigee height: | 905 km |
apogee height: | 913 km |
right ascension of ascending node: | 71.7071° |
argument of perigee: | 33.0838° |
revolutions per day: | 13.95523942 |
mean anomaly at epoch: | 327.0695° |
orbit number at epoch: | 50276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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