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 56531U 26145.39224175 +.00000000 +00000-0 +38862-4 0 00005
2 56531 43.0054 125.1583 0001286 279.8658 80.2049 15.27579886 06
| Epoch (UTC): | 25 May 2026 09:24:49 |
| Eccentricity: | 0.0001286 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.1583° |
| argument of perigee: | 279.8658° |
| revolutions per day: | 15.27579886 |
| mean anomaly at epoch: | 80.2049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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