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 05918U 26159.34604066 +.00000000 +00000-0 +27141-4 0 00007
2 05918 81.2386 34.0370 0059206 113.3509 247.3903 14.06315339 07
| Epoch (UTC): | 08 June 2026 08:18:17 |
| Eccentricity: | 0.0059206 |
| inclination: | 81.2386° |
| perigee height: | 829 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 34.0370° |
| argument of perigee: | 113.3509° |
| revolutions per day: | 14.06315339 |
| mean anomaly at epoch: | 247.3903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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