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 00544U 26132.44355029 +.00000000 +00000-0 +26220-3 0 00007
2 00544 66.8741 301.9786 0191989 287.7305 96.2345 13.56193991 06
| Epoch (UTC): | 12 May 2026 10:38:42 |
| Eccentricity: | 0.0191989 |
| inclination: | 66.8741° |
| perigee height: | 907 km |
| apogee height: | 1192 km |
| right ascension of ascending node: | 301.9786° |
| argument of perigee: | 287.7305° |
| revolutions per day: | 13.56193991 |
| mean anomaly at epoch: | 96.2345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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