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 43574U 26145.48706132 +.00000000 +00000-0 +59686-4 0 00003
2 43574 86.3970 66.2960 0002119 83.2493 276.8944 14.34219780 08
| Epoch (UTC): | 25 May 2026 11:41:22 |
| Eccentricity: | 0.0002119 |
| inclination: | 86.3970° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2960° |
| argument of perigee: | 83.2493° |
| revolutions per day: | 14.34219780 |
| mean anomaly at epoch: | 276.8944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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