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 68109U 26145.63158552 +.00000000 +00000-0 +56255-3 0 00006
2 68109 97.2837 106.2388 0001982 92.4411 267.7058 15.33451062 06
| Epoch (UTC): | 25 May 2026 15:09:28 |
| Eccentricity: | 0.0001982 |
| inclination: | 97.2837° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.2388° |
| argument of perigee: | 92.4411° |
| revolutions per day: | 15.33451062 |
| mean anomaly at epoch: | 267.7058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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