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 58285U 26145.23173426 +.00000000 +00000-0 +51493-3 0 00002
2 58285 97.3910 236.5653 0006178 213.9153 146.1708 15.55683214 02
| Epoch (UTC): | 25 May 2026 05:33:41 |
| Eccentricity: | 0.0006178 |
| inclination: | 97.3910° |
| perigee height: | 396 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 236.5653° |
| argument of perigee: | 213.9153° |
| revolutions per day: | 15.55683214 |
| mean anomaly at epoch: | 146.1708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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