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 45531U 26145.47100907 +.00000000 +00000-0 +49879-3 0 00007
2 45531 53.0423 63.8250 0004723 92.8895 267.2662 15.71202520 04
| Epoch (UTC): | 25 May 2026 11:18:15 |
| Eccentricity: | 0.0004723 |
| inclination: | 53.0423° |
| perigee height: | 352 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 63.8250° |
| argument of perigee: | 92.8895° |
| revolutions per day: | 15.71202520 |
| mean anomaly at epoch: | 267.2662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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