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 21060.15916839 -.00000041 00000-0 27859-4 0 9993
2 116 66.8099 300.6569 0076785 193.9859 165.9095 13.91784483 28029
| Epoch (UTC): | 01 March 2021 03:49:12 |
| Eccentricity: | 0.0076785 |
| inclination: | 66.8099° |
| perigee height: | 866 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 300.6569° |
| argument of perigee: | 193.9859° |
| revolutions per day: | 13.91784483 |
| mean anomaly at epoch: | 165.9095° |
| orbit number at epoch: | 2802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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