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 21018.76752757 -.00000085 00000-0 -62338-5 0 9991
2 00116 66.8084 41.8450 0079943 221.8978 137.5967 13.91781773 21786
Epoch (UTC): | 18 January 2021 18:25:14 |
Eccentricity: | 0.0079943 |
inclination: | 66.8084° |
perigee height: | 864 km |
apogee height: | 981 km |
right ascension of ascending node: | 41.8450° |
argument of perigee: | 221.8978° |
revolutions per day: | 13.91781773 |
mean anomaly at epoch: | 137.5967° |
orbit number at epoch: | 2178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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