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 68355U 26145.44869399 +.00000000 +00000-0 +25314-4 0 00009
2 68355 54.9743 128.7981 0010806 83.1787 277.0440 14.72898999 06
| Epoch (UTC): | 25 May 2026 10:46:07 |
| Eccentricity: | 0.0010806 |
| inclination: | 54.9743° |
| perigee height: | 644 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 128.7981° |
| argument of perigee: | 83.1787° |
| revolutions per day: | 14.72898999 |
| mean anomaly at epoch: | 277.0440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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