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 62726U 26145.43865589 +.00000000 +00000-0 +20075-3 0 00009
2 62726 97.4238 218.8299 0008798 7.1861 352.9499 15.20970699 01
| Epoch (UTC): | 25 May 2026 10:31:39 |
| Eccentricity: | 0.0008798 |
| inclination: | 97.4238° |
| perigee height: | 497 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 218.8299° |
| argument of perigee: | 7.1861° |
| revolutions per day: | 15.20970699 |
| mean anomaly at epoch: | 352.9499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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