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 65043U 26145.53710661 +.00000000 +00000-0 +75841-4 0 00007
2 65043 50.0011 347.1828 0000468 45.9299 314.1611 13.29323931 09
| Epoch (UTC): | 25 May 2026 12:53:26 |
| Eccentricity: | 0.0000468 |
| inclination: | 50.0011° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 347.1828° |
| argument of perigee: | 45.9299° |
| revolutions per day: | 13.29323931 |
| mean anomaly at epoch: | 314.1611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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