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 55569U 26145.47751468 +.00000000 +00000-0 +77916-5 0 00008
2 55569 43.0030 295.2052 0002022 275.1849 84.8771 15.25907911 04
| Epoch (UTC): | 25 May 2026 11:27:37 |
| Eccentricity: | 0.0002022 |
| inclination: | 43.0030° |
| perigee height: | 487 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 295.2052° |
| argument of perigee: | 275.1849° |
| revolutions per day: | 15.25907911 |
| mean anomaly at epoch: | 84.8771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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