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 45142U 26145.45101507 +.00000000 +00000-0 +55511-3 0 00000
2 45142 87.8854 40.8043 0001306 78.0891 282.0382 13.10377565 03
| Epoch (UTC): | 25 May 2026 10:49:27 |
| Eccentricity: | 0.0001306 |
| inclination: | 87.8854° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8043° |
| argument of perigee: | 78.0891° |
| revolutions per day: | 13.10377565 |
| mean anomaly at epoch: | 282.0382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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