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 59571U 26145.66668980 +.00000000 +00000-0 -86872-5 0 00004
2 59571 42.9997 293.8714 0001450 273.8200 317.5279 15.27577481 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001450 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.8714° |
| argument of perigee: | 273.8200° |
| revolutions per day: | 15.27577481 |
| mean anomaly at epoch: | 317.5279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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