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 32379U 07060B 23160.79603925 .00007747 00000-0 15212-2 0 9998
2 32379 60.7722 225.3444 5021227 214.3599 99.6692 5.57060511 78068
| Epoch (UTC): | 09 June 2023 19:06:17 |
| Eccentricity: | 0.5021227 |
| inclination: | 60.7722° |
| perigee height: | 314 km |
| apogee height: | 13813 km |
| right ascension of ascending node: | 225.3444° |
| argument of perigee: | 214.3599° |
| revolutions per day: | 5.57060511 |
| mean anomaly at epoch: | 99.6692° |
| orbit number at epoch: | 7806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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