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 07646U 26145.60796536 +.00000000 +00000-0 +59599-5 0 00008
2 07646 49.8223 193.7227 0205586 348.4476 11.1739 13.82350173 01
| Epoch (UTC): | 25 May 2026 14:35:28 |
| Eccentricity: | 0.0205586 |
| inclination: | 49.8223° |
| perigee height: | 805 km |
| apogee height: | 1106 km |
| right ascension of ascending node: | 193.7227° |
| argument of perigee: | 348.4476° |
| revolutions per day: | 13.82350173 |
| mean anomaly at epoch: | 11.1739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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