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 66056U 26145.44221808 +.00000000 +00000-0 +58433-3 0 00009
2 66056 97.4254 213.6706 0003764 146.1598 213.9879 15.21417202 09
| Epoch (UTC): | 25 May 2026 10:36:47 |
| Eccentricity: | 0.0003764 |
| inclination: | 97.4254° |
| perigee height: | 499 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 213.6706° |
| argument of perigee: | 146.1598° |
| revolutions per day: | 15.21417202 |
| mean anomaly at epoch: | 213.9879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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