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 21023.72590368 -.00000069 00000-0 63307-5 0 9999
2 00116 66.8104 29.7226 0079625 218.6391 140.8975 13.91781926 22478
Epoch (UTC): | 23 January 2021 17:25:18 |
Eccentricity: | 0.0079625 |
inclination: | 66.8104° |
perigee height: | 864 km |
apogee height: | 980 km |
right ascension of ascending node: | 29.7226° |
argument of perigee: | 218.6391° |
revolutions per day: | 13.91781926 |
mean anomaly at epoch: | 140.8975° |
orbit number at epoch: | 2247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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