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 32789U 08021G 22178.52930001 .00008652 00000-0 47920-3 0 9996
2 32789 97.3378 204.4638 0008035 291.5705 68.4671 15.14023528773459
| Epoch (UTC): | 27 June 2022 12:42:11 |
| Eccentricity: | 0.0008035 |
| inclination: | 97.3378° |
| perigee height: | 518 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 204.4638° |
| argument of perigee: | 291.5705° |
| revolutions per day: | 15.14023528 |
| mean anomaly at epoch: | 68.4671° |
| orbit number at epoch: | 77345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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