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 is defined by the following mean orbital elements,
1 43765U 26145.57197815 +.00000000 +00000-0 +25597-3 0 00000
2 43765 97.3932 198.1060 0034983 8.1654 352.0146 15.24319805 05
| Epoch (UTC): | 25 May 2026 13:43:38 |
| Eccentricity: | 0.0034983 |
| inclination: | 97.3932° |
| perigee height: | 469 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 198.1060° |
| argument of perigee: | 8.1654° |
| revolutions per day: | 15.24319805 |
| mean anomaly at epoch: | 352.0146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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