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 57809U 26145.33628815 +.00000000 +00000-0 -15861-3 0 00001
2 57809 43.0012 161.0498 0001676 279.6179 80.4484 15.27582576 07
| Epoch (UTC): | 25 May 2026 08:04:15 |
| Eccentricity: | 0.0001676 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.0498° |
| argument of perigee: | 279.6179° |
| revolutions per day: | 15.27582576 |
| mean anomaly at epoch: | 80.4484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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