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 68585U 26145.58335647 +.00000000 +00000-0 -71831-1 0 00006
2 68585 51.8870 287.6313 0007954 305.0892 6.5713 15.11148468 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007954 |
| inclination: | 51.8870° |
| perigee height: | 527 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 287.6313° |
| argument of perigee: | 305.0892° |
| revolutions per day: | 15.11148468 |
| mean anomaly at epoch: | 6.5713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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