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 is defined by the following mean orbital elements,
1 43640U 98067PQ 21177.48090856 .06251270 12411-4 46174-3 0 9996
2 43640 51.6078 176.1291 0003401 286.8094 73.2559 16.39860287155785
| Epoch (UTC): | 26 June 2021 11:32:30 |
| Eccentricity: | 0.0003401 |
| inclination: | 51.6078° |
| perigee height: | 164 km |
| apogee height: | 168 km |
| right ascension of ascending node: | 176.1291° |
| argument of perigee: | 286.8094° |
| revolutions per day: | 16.39860287 |
| mean anomaly at epoch: | 73.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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