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 68062U 26145.58335647 +.00000000 +00000-0 +17958-2 0 00006
2 68062 53.1594 51.0914 0001242 97.5878 274.9596 15.34354438 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001242 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 51.0914° |
| argument of perigee: | 97.5878° |
| revolutions per day: | 15.34354438 |
| mean anomaly at epoch: | 274.9596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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