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 45158U 26145.40454646 +.00000000 +00000-0 +64442-3 0 00000
2 45158 87.8857 40.8008 0001827 81.9856 278.1478 13.10370442 05
| Epoch (UTC): | 25 May 2026 09:42:32 |
| Eccentricity: | 0.0001827 |
| inclination: | 87.8857° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8008° |
| argument of perigee: | 81.9856° |
| revolutions per day: | 13.10370442 |
| mean anomaly at epoch: | 278.1478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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