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 66822U 26145.37989979 +.00000000 +00000-0 +47220-4 0 00005
2 66822 70.0003 141.0824 0003799 263.0789 96.9938 14.98330706 04
| Epoch (UTC): | 25 May 2026 09:07:03 |
| Eccentricity: | 0.0003799 |
| inclination: | 70.0003° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.0824° |
| argument of perigee: | 263.0789° |
| revolutions per day: | 14.98330706 |
| mean anomaly at epoch: | 96.9938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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