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 06779U 26074.61982733 +.00000000 +00000-0 -15173-2 0 00000
2 06779 28.1478 52.1476 7175447 99.2367 341.1785 2.19673474 09
| Epoch (UTC): | 15 March 2026 14:52:33 |
| Eccentricity: | 0.7175447 |
| inclination: | 28.1478° |
| perigee height: | 682 km |
| apogee height: | 36555 km |
| right ascension of ascending node: | 52.1476° |
| argument of perigee: | 99.2367° |
| revolutions per day: | 2.19673474 |
| mean anomaly at epoch: | 341.1785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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