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 68418U 26145.57640264 +.00000000 +00000-0 +25054-3 0 00001
2 68418 97.4570 104.4523 0003436 46.4587 313.6932 15.18749239 06
| Epoch (UTC): | 25 May 2026 13:50:01 |
| Eccentricity: | 0.0003436 |
| inclination: | 97.4570° |
| perigee height: | 507 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 104.4523° |
| argument of perigee: | 46.4587° |
| revolutions per day: | 15.18749239 |
| mean anomaly at epoch: | 313.6932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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