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 22219.37166466 -.00000039 00000-0 28866-4 0 9993
2 00116 66.8097 99.0863 0076471 186.8059 173.1990 13.91839757100478
| Epoch (UTC): | 07 August 2022 08:55:11 |
| Eccentricity: | 0.0076471 |
| inclination: | 66.8097° |
| perigee height: | 866 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 99.0863° |
| argument of perigee: | 186.8059° |
| revolutions per day: | 13.91839757 |
| mean anomaly at epoch: | 173.1990° |
| orbit number at epoch: | 10047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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