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 56693U 26145.21759329 +.00000000 +00000-0 +23586-3 0 00005
2 56693 43.0029 209.1235 0001388 265.3870 94.6823 15.27584900 05
| Epoch (UTC): | 25 May 2026 05:13:20 |
| Eccentricity: | 0.0001388 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.1235° |
| argument of perigee: | 265.3870° |
| revolutions per day: | 15.27584900 |
| mean anomaly at epoch: | 94.6823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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