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 68575U 26145.58335647 +.00000000 +00000-0 -78424-2 0 00001
2 68575 51.8997 293.1061 0002795 110.9403 132.1283 14.80692662 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002795 |
| inclination: | 51.8997° |
| perigee height: | 625 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 293.1061° |
| argument of perigee: | 110.9403° |
| revolutions per day: | 14.80692662 |
| mean anomaly at epoch: | 132.1283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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