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 58485U 26145.58210487 +.00000000 +00000-0 +84101-4 0 00004
2 58485 43.0027 349.5947 0001045 273.8314 86.2418 15.27580726 09
| Epoch (UTC): | 25 May 2026 13:58:13 |
| Eccentricity: | 0.0001045 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.5947° |
| argument of perigee: | 273.8314° |
| revolutions per day: | 15.27580726 |
| mean anomaly at epoch: | 86.2418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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