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 57609U 26145.60919845 +.00000000 +00000-0 +21852-4 0 00002
2 57609 43.0072 6.8807 0002054 244.8195 115.2444 15.27580418 00
| Epoch (UTC): | 25 May 2026 14:37:14 |
| Eccentricity: | 0.0002054 |
| inclination: | 43.0072° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.8807° |
| argument of perigee: | 244.8195° |
| revolutions per day: | 15.27580418 |
| mean anomaly at epoch: | 115.2444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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