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 68885U 26145.58335647 +.00000000 +00000-0 -49630-2 0 00002
2 68885 51.8914 355.7369 0014238 239.8510 270.0888 14.94778427 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0014238 |
| inclination: | 51.8914° |
| perigee height: | 573 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 355.7369° |
| argument of perigee: | 239.8510° |
| revolutions per day: | 14.94778427 |
| mean anomaly at epoch: | 270.0888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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