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 59291U 26145.51516612 +.00000000 +00000-0 +33638-3 0 00000
2 59291 49.9905 80.1648 0001987 233.9713 126.1066 15.43028443 00
| Epoch (UTC): | 25 May 2026 12:21:50 |
| Eccentricity: | 0.0001987 |
| inclination: | 49.9905° |
| perigee height: | 436 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 80.1648° |
| argument of perigee: | 233.9713° |
| revolutions per day: | 15.43028443 |
| mean anomaly at epoch: | 126.1066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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