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 59906U 26145.41758810 +.00000000 +00000-0 +27874-5 0 00007
2 59906 43.0021 44.9370 0000809 278.6310 81.4450 15.27573004 08
| Epoch (UTC): | 25 May 2026 10:01:19 |
| Eccentricity: | 0.0000809 |
| inclination: | 43.0021° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.9370° |
| argument of perigee: | 278.6310° |
| revolutions per day: | 15.27573004 |
| mean anomaly at epoch: | 81.4450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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