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 58806U 26145.25266924 +.00000000 +00000-0 +13007-3 0 00008
2 58806 43.0022 92.9910 0001461 259.7245 100.3442 15.27604774 03
| Epoch (UTC): | 25 May 2026 06:03:50 |
| Eccentricity: | 0.0001461 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 92.9910° |
| argument of perigee: | 259.7245° |
| revolutions per day: | 15.27604774 |
| mean anomaly at epoch: | 100.3442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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