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 68357U 26145.35934937 +.00000000 +00000-0 +18840-3 0 00007
2 68357 54.9844 129.0194 0012898 88.7969 271.4507 14.73562343 00
| Epoch (UTC): | 25 May 2026 08:37:27 |
| Eccentricity: | 0.0012898 |
| inclination: | 54.9844° |
| perigee height: | 641 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 129.0194° |
| argument of perigee: | 88.7969° |
| revolutions per day: | 14.73562343 |
| mean anomaly at epoch: | 271.4507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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