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 45071U 26145.57193623 +.00000000 +00000-0 +11896-2 0 00001
2 45071 53.1572 259.3505 0002523 264.9881 95.0835 15.36045586 04
| Epoch (UTC): | 25 May 2026 13:43:35 |
| Eccentricity: | 0.0002523 |
| inclination: | 53.1572° |
| perigee height: | 456 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 259.3505° |
| argument of perigee: | 264.9881° |
| revolutions per day: | 15.36045586 |
| mean anomaly at epoch: | 95.0835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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