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 32289U 07055A 24357.86300923 .00004551 00000-0 51032-3 0 9992
2 32289 97.8718 21.4748 0001791 81.6384 278.5035 14.87306110925298
| Epoch (UTC): | 22 December 2024 20:42:43 |
| Eccentricity: | 0.0001791 |
| inclination: | 97.8718° |
| perigee height: | 605 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 21.4748° |
| argument of perigee: | 81.6384° |
| revolutions per day: | 14.87306110 |
| mean anomaly at epoch: | 278.5035° |
| orbit number at epoch: | 92529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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