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 58866U 26145.43835684 +.00000000 +00000-0 -20868-4 0 00004
2 58866 43.0004 175.1852 0001259 272.5810 87.4898 15.27573898 06
| Epoch (UTC): | 25 May 2026 10:31:14 |
| Eccentricity: | 0.0001259 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.1852° |
| argument of perigee: | 272.5810° |
| revolutions per day: | 15.27573898 |
| mean anomaly at epoch: | 87.4898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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