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 58063U 26145.48272716 +.00000000 +00000-0 +86398-4 0 00008
2 58063 43.0040 313.4347 0001688 266.7406 93.3253 15.27576128 03
| Epoch (UTC): | 25 May 2026 11:35:07 |
| Eccentricity: | 0.0001688 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.4347° |
| argument of perigee: | 266.7406° |
| revolutions per day: | 15.27576128 |
| mean anomaly at epoch: | 93.3253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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