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 57064U 26145.38508138 +.00000000 +00000-0 +21228-4 0 00008
2 57064 43.0052 37.3726 0001155 229.5566 130.5185 15.27578480 03
| Epoch (UTC): | 25 May 2026 09:14:31 |
| Eccentricity: | 0.0001155 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.3726° |
| argument of perigee: | 229.5566° |
| revolutions per day: | 15.27578480 |
| mean anomaly at epoch: | 130.5185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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