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 56020U 26144.86893175 +.00000000 +00000-0 +42106-4 0 00007
2 56020 43.0034 335.2174 0001607 253.4250 106.6426 15.27578502 06
| Epoch (UTC): | 24 May 2026 20:51:15 |
| Eccentricity: | 0.0001607 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.2174° |
| argument of perigee: | 253.4250° |
| revolutions per day: | 15.27578502 |
| mean anomaly at epoch: | 106.6426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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