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 59290U 26144.92667330 +.00000000 +00000-0 +33179-3 0 00007
2 59290 49.9891 82.9469 0002039 238.8287 121.2476 15.43046339 08
| Epoch (UTC): | 24 May 2026 22:14:24 |
| Eccentricity: | 0.0002039 |
| inclination: | 49.9891° |
| perigee height: | 436 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 82.9469° |
| argument of perigee: | 238.8287° |
| revolutions per day: | 15.43046339 |
| mean anomaly at epoch: | 121.2476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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