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 56695U 26145.54838508 +.00000000 +00000-0 +10252-4 0 00007
2 56695 43.0019 207.2864 0000988 285.8530 74.2213 15.27576287 04
| Epoch (UTC): | 25 May 2026 13:09:40 |
| Eccentricity: | 0.0000988 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.2864° |
| argument of perigee: | 285.8530° |
| revolutions per day: | 15.27576287 |
| mean anomaly at epoch: | 74.2213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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