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 64325U 26145.41980527 +.00000000 +00000-0 +13183-2 0 00005
2 64325 43.0005 286.5659 0001917 249.5162 110.5500 15.70947342 06
| Epoch (UTC): | 25 May 2026 10:04:31 |
| Eccentricity: | 0.0001917 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 286.5659° |
| argument of perigee: | 249.5162° |
| revolutions per day: | 15.70947342 |
| mean anomaly at epoch: | 110.5500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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