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 45424U 26145.41026029 +.00000000 +00000-0 +61391-3 0 00007
2 45424 87.8914 25.6027 0001861 76.2143 283.9192 13.11418239 06
| Epoch (UTC): | 25 May 2026 09:50:46 |
| Eccentricity: | 0.0001861 |
| inclination: | 87.8914° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6027° |
| argument of perigee: | 76.2143° |
| revolutions per day: | 13.11418239 |
| mean anomaly at epoch: | 283.9192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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