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 22221.38367660 -.00000021 00000-0 42689-4 0 9996
2 116 66.8095 94.1669 0076306 185.3996 174.6269 13.91839943101256
| Epoch (UTC): | 09 August 2022 09:12:29 |
| Eccentricity: | 0.0076306 |
| inclination: | 66.8095° |
| perigee height: | 866 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 94.1669° |
| argument of perigee: | 185.3996° |
| revolutions per day: | 13.91839943 |
| mean anomaly at epoch: | 174.6269° |
| orbit number at epoch: | 10125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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