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 68068U 26145.46392963 +.00000000 +00000-0 +75252-3 0 00005
2 68068 53.1594 53.1990 0001146 84.3198 275.7935 15.34403173 08
| Epoch (UTC): | 25 May 2026 11:08:03 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 53.1990° |
| argument of perigee: | 84.3198° |
| revolutions per day: | 15.34403173 |
| mean anomaly at epoch: | 275.7935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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