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 53856U 26145.66668980 +.00000000 +00000-0 +85479-2 0 00002
2 53856 53.2170 290.9384 0001024 69.8144 212.1861 15.52822934 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.2170° |
| perigee height: | 408 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 290.9384° |
| argument of perigee: | 69.8144° |
| revolutions per day: | 15.52822934 |
| mean anomaly at epoch: | 212.1861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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