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 32791U 08021J 23153.42974871 .00005023 00000-0 44573-3 0 9995
2 32791 97.6547 124.9787 0013817 99.5946 260.6837 14.96545048819536
| Epoch (UTC): | 02 June 2023 10:18:50 |
| Eccentricity: | 0.0013817 |
| inclination: | 97.6547° |
| perigee height: | 568 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 124.9787° |
| argument of perigee: | 99.5946° |
| revolutions per day: | 14.96545048 |
| mean anomaly at epoch: | 260.6837° |
| orbit number at epoch: | 81953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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