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 59366U 26145.56391988 +.00000000 +00000-0 +37031-4 0 00007
2 59366 43.0030 185.3802 0001375 274.9010 85.1685 15.27579600 02
| Epoch (UTC): | 25 May 2026 13:32:02 |
| Eccentricity: | 0.0001375 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.3802° |
| argument of perigee: | 274.9010° |
| revolutions per day: | 15.27579600 |
| mean anomaly at epoch: | 85.1685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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