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 45161U 26145.45614256 +.00000000 +00000-0 +14745-2 0 00004
2 45161 87.8855 40.8046 0001697 72.4569 287.6744 13.10376549 05
| Epoch (UTC): | 25 May 2026 10:56:50 |
| Eccentricity: | 0.0001697 |
| inclination: | 87.8855° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8046° |
| argument of perigee: | 72.4569° |
| revolutions per day: | 13.10376549 |
| mean anomaly at epoch: | 287.6744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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