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 05398U 26145.57420486 +.00000000 +00000-0 +15531-3 0 00000
2 05398 87.6216 345.0931 0058105 309.4171 50.1892 14.37839400 00
| Epoch (UTC): | 25 May 2026 13:46:51 |
| Eccentricity: | 0.0058105 |
| inclination: | 87.6216° |
| perigee height: | 724 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 345.0931° |
| argument of perigee: | 309.4171° |
| revolutions per day: | 14.37839400 |
| mean anomaly at epoch: | 50.1892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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