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 56759U 26145.60935948 +.00000000 +00000-0 +00000-0 0 00007
2 56759 2.2175 245.3410 0003368 47.6566 299.0695 1.00276720 09
| Epoch (UTC): | 25 May 2026 14:37:28 |
| Eccentricity: | 0.0003368 |
| inclination: | 2.2175° |
| perigee height: | 35771 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 245.3410° |
| argument of perigee: | 47.6566° |
| revolutions per day: | 1.00276720 |
| mean anomaly at epoch: | 299.0695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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