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 68966U 26145.58335647 +.00000000 +00000-0 -27160-1 0 00005
2 68966 53.1595 268.1333 0001019 56.3605 15.7935 15.59128832 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.1595° |
| perigee height: | 389 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 268.1333° |
| argument of perigee: | 56.3605° |
| revolutions per day: | 15.59128832 |
| mean anomaly at epoch: | 15.7935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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