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 59810U 26145.63060625 +.00000000 +00000-0 +27856-3 0 00003
2 59810 97.5344 224.8684 0003157 41.2571 318.8897 15.11116831 09
| Epoch (UTC): | 25 May 2026 15:08:04 |
| Eccentricity: | 0.0003157 |
| inclination: | 97.5344° |
| perigee height: | 531 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 224.8684° |
| argument of perigee: | 41.2571° |
| revolutions per day: | 15.11116831 |
| mean anomaly at epoch: | 318.8897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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