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 00116U 61015A 21019.77357485 -.00000078 00000-0 -42316-6 0 9999
2 00116 66.8084 39.3854 0079888 221.2309 138.2720 13.91781817 21926
Epoch (UTC): | 19 January 2021 18:33:56 |
Eccentricity: | 0.0079888 |
inclination: | 66.8084° |
perigee height: | 864 km |
apogee height: | 981 km |
right ascension of ascending node: | 39.3854° |
argument of perigee: | 221.2309° |
revolutions per day: | 13.91781817 |
mean anomaly at epoch: | 138.2720° |
orbit number at epoch: | 2192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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