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 68345U 26145.58335647 +.00000000 +00000-0 -52386-1 0 00004
2 68345 53.1592 346.6205 0001299 112.1883 161.0197 15.38948397 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.1592° |
| perigee height: | 448 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 346.6205° |
| argument of perigee: | 112.1883° |
| revolutions per day: | 15.38948397 |
| mean anomaly at epoch: | 161.0197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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