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 58849U 26145.60380362 +.00000000 +00000-0 +26908-3 0 00001
2 58849 58.6866 308.9608 0437671 79.3437 285.6552 14.39407487 00
| Epoch (UTC): | 25 May 2026 14:29:28 |
| Eccentricity: | 0.0437671 |
| inclination: | 58.6866° |
| perigee height: | 448 km |
| apogee height: | 1073 km |
| right ascension of ascending node: | 308.9608° |
| argument of perigee: | 79.3437° |
| revolutions per day: | 14.39407487 |
| mean anomaly at epoch: | 285.6552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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