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 66068U 26145.57306354 +.00000000 +00000-0 +57591-3 0 00000
2 66068 53.1590 248.0854 0002624 97.2727 262.8572 15.30217338 05
| Epoch (UTC): | 25 May 2026 13:45:12 |
| Eccentricity: | 0.0002624 |
| inclination: | 53.1590° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 248.0854° |
| argument of perigee: | 97.2727° |
| revolutions per day: | 15.30217338 |
| mean anomaly at epoch: | 262.8572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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