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 32785U 08021C 23080.80631017 .00005959 00000-0 60047-3 0 9993
2 32785 97.6972 48.7295 0013749 41.1232 319.1020 14.91435961807799
| Epoch (UTC): | 21 March 2023 19:21:05 |
| Eccentricity: | 0.0013749 |
| inclination: | 97.6972° |
| perigee height: | 584 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 48.7295° |
| argument of perigee: | 41.1232° |
| revolutions per day: | 14.91435961 |
| mean anomaly at epoch: | 319.1020° |
| orbit number at epoch: | 80779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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