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 45155U 26145.42552800 +.00000000 +00000-0 +13336-2 0 00005
2 45155 87.8910 25.5956 0001827 81.8970 278.2365 13.11414922 09
| Epoch (UTC): | 25 May 2026 10:12:45 |
| Eccentricity: | 0.0001827 |
| inclination: | 87.8910° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5956° |
| argument of perigee: | 81.8970° |
| revolutions per day: | 13.11414922 |
| mean anomaly at epoch: | 278.2365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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