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 58745U 26145.45870634 +.00000000 +00000-0 +23896-3 0 00008
2 58745 43.0039 146.2855 0001771 295.4501 64.6167 15.27582713 04
| Epoch (UTC): | 25 May 2026 11:00:32 |
| Eccentricity: | 0.0001771 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.2855° |
| argument of perigee: | 295.4501° |
| revolutions per day: | 15.27582713 |
| mean anomaly at epoch: | 64.6167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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