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 58282U 26145.58091258 +.00000000 +00000-0 +39871-3 0 00005
2 58282 97.3814 235.5148 0004914 206.9700 153.1299 15.53202671 01
| Epoch (UTC): | 25 May 2026 13:56:30 |
| Eccentricity: | 0.0004914 |
| inclination: | 97.3814° |
| perigee height: | 404 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 235.5148° |
| argument of perigee: | 206.9700° |
| revolutions per day: | 15.53202671 |
| mean anomaly at epoch: | 153.1299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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