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 58168U 26145.37491823 +.00000000 +00000-0 +23743-4 0 00009
2 58168 53.1608 223.1745 0000949 72.5642 287.5462 15.30194800 00
| Epoch (UTC): | 25 May 2026 08:59:52 |
| Eccentricity: | 0.0000949 |
| inclination: | 53.1608° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.1745° |
| argument of perigee: | 72.5642° |
| revolutions per day: | 15.30194800 |
| mean anomaly at epoch: | 287.5462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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