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 42941U 17056A 20353.50606290 0.00000000 00000-0 00000-0 0 03
2 42941 63.6418 26.2390 7176759 266.5740 93.4260 2.00623300 04
Epoch (UTC): | 18 December 2020 12:08:43 |
Eccentricity: | 0.7176759 |
inclination: | 63.6418° |
perigee height: | 1119 km |
apogee height: | 39234 km |
right ascension of ascending node: | 26.2390° |
argument of perigee: | 266.5740° |
revolutions per day: | 2.00623300 |
mean anomaly at epoch: | 93.4260° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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