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 56934U 26145.65611904 +.00000000 +00000-0 +22160-3 0 00004
2 56934 97.6188 285.8779 0006944 73.3662 286.8342 15.34294103 09
| Epoch (UTC): | 25 May 2026 15:44:48 |
| Eccentricity: | 0.0006944 |
| inclination: | 97.6188° |
| perigee height: | 458 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 285.8779° |
| argument of perigee: | 73.3662° |
| revolutions per day: | 15.34294103 |
| mean anomaly at epoch: | 286.8342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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