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 58166U 26145.59408193 +.00000000 +00000-0 +26095-4 0 00002
2 58166 53.1605 222.4051 0000974 106.1936 253.9172 15.30187822 06
| Epoch (UTC): | 25 May 2026 14:15:28 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.4051° |
| argument of perigee: | 106.1936° |
| revolutions per day: | 15.30187822 |
| mean anomaly at epoch: | 253.9172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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