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 22220.48665265 .00013423 00000-0 72489-3 0 9996
2 32789 97.3375 244.9325 0011729 137.3013 222.9133 15.14778107779907
| Epoch (UTC): | 08 August 2022 11:40:46 |
| Eccentricity: | 0.0011729 |
| inclination: | 97.3375° |
| perigee height: | 513 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 244.9325° |
| argument of perigee: | 137.3013° |
| revolutions per day: | 15.14778107 |
| mean anomaly at epoch: | 222.9133° |
| orbit number at epoch: | 77990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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