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 116U 61015A 21063.46474749 -.00000057 00000-0 15328-4 0 9994
2 116 66.8092 292.5758 0076506 191.7077 168.2227 13.91784639 28486
Epoch (UTC): | 04 March 2021 11:09:14 |
Eccentricity: | 0.0076506 |
inclination: | 66.8092° |
perigee height: | 866 km |
apogee height: | 978 km |
right ascension of ascending node: | 292.5758° |
argument of perigee: | 191.7077° |
revolutions per day: | 13.91784639 |
mean anomaly at epoch: | 168.2227° |
orbit number at epoch: | 2848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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