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 45163U 26145.39943058 +.00000000 +00000-0 +13901-2 0 00007
2 45163 87.8858 40.8006 0001432 72.7049 287.4235 13.10370420 04
| Epoch (UTC): | 25 May 2026 09:35:10 |
| Eccentricity: | 0.0001432 |
| inclination: | 87.8858° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8006° |
| argument of perigee: | 72.7049° |
| revolutions per day: | 13.10370420 |
| mean anomaly at epoch: | 287.4235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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