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 22221.59924929 -.00000019 00000-0 44749-4 0 9992
2 00116 66.8095 93.6399 0076292 185.2489 174.7799 13.91839975100781
| Epoch (UTC): | 09 August 2022 14:22:55 |
| Eccentricity: | 0.0076292 |
| inclination: | 66.8095° |
| perigee height: | 866 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 93.6399° |
| argument of perigee: | 185.2489° |
| revolutions per day: | 13.91839975 |
| mean anomaly at epoch: | 174.7799° |
| orbit number at epoch: | 10078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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