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 43569U 26145.52512171 +.00000000 +00000-0 +10521-5 0 00006
2 43569 86.3970 66.2707 0002249 87.2289 272.9164 14.34217373 09
| Epoch (UTC): | 25 May 2026 12:36:10 |
| Eccentricity: | 0.0002249 |
| inclination: | 86.3970° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2707° |
| argument of perigee: | 87.2289° |
| revolutions per day: | 14.34217373 |
| mean anomaly at epoch: | 272.9164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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