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 68794U 26145.36417227 +.00000000 +00000-0 +29338-3 0 00005
2 68794 97.5039 295.2274 0013381 169.1691 190.9828 15.07065345 02
| Epoch (UTC): | 25 May 2026 08:44:24 |
| Eccentricity: | 0.0013381 |
| inclination: | 97.5039° |
| perigee height: | 536 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 295.2274° |
| argument of perigee: | 169.1691° |
| revolutions per day: | 15.07065345 |
| mean anomaly at epoch: | 190.9828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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