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 21333.51392384 -.00000050 00000-0 20504-4 0 9999
2 116 66.8105 352.3982 0076208 352.3168 7.6737 13.91803127 66062
| Epoch (UTC): | 29 November 2021 12:20:03 |
| Eccentricity: | 0.0076208 |
| inclination: | 66.8105° |
| perigee height: | 866 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 352.3982° |
| argument of perigee: | 352.3168° |
| revolutions per day: | 13.91803127 |
| mean anomaly at epoch: | 7.6737° |
| orbit number at epoch: | 6606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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