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 40012U 14033C 22179.51022851 .00000865 00000-0 13241-3 0 9996
2 40012 97.6615 6.8829 0058748 122.4969 238.1937 14.74932159431614
| Epoch (UTC): | 28 June 2022 12:14:43 |
| Eccentricity: | 0.0058748 |
| inclination: | 97.6615° |
| perigee height: | 604 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 6.8829° |
| argument of perigee: | 122.4969° |
| revolutions per day: | 14.74932159 |
| mean anomaly at epoch: | 238.1937° |
| orbit number at epoch: | 43161 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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