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 43491U 26145.52822512 +.00000000 +00000-0 +00000-0 0 00009
2 43491 2.9756 79.3298 0001566 145.4815 287.9007 1.00271907 06
| Epoch (UTC): | 25 May 2026 12:40:38 |
| Eccentricity: | 0.0001566 |
| inclination: | 2.9756° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 79.3298° |
| argument of perigee: | 145.4815° |
| revolutions per day: | 1.00271907 |
| mean anomaly at epoch: | 287.9007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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