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 68256U 26145.45211781 +.00000000 +00000-0 +73106-3 0 00007
2 68256 53.1572 300.4056 0000525 120.8274 239.2779 15.30225639 01
| Epoch (UTC): | 25 May 2026 10:51:02 |
| Eccentricity: | 0.0000525 |
| inclination: | 53.1572° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 300.4056° |
| argument of perigee: | 120.8274° |
| revolutions per day: | 15.30225639 |
| mean anomaly at epoch: | 239.2779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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