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 58006U 26145.53810360 +.00000000 +00000-0 +84991-3 0 00000
2 58006 43.0040 327.5105 0003963 287.6693 72.3727 15.29639452 01
| Epoch (UTC): | 25 May 2026 12:54:52 |
| Eccentricity: | 0.0003963 |
| inclination: | 43.0040° |
| perigee height: | 474 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 327.5105° |
| argument of perigee: | 287.6693° |
| revolutions per day: | 15.29639452 |
| mean anomaly at epoch: | 72.3727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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