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 54163U 26145.38528869 +.00000000 +00000-0 +40160-4 0 00004
2 54163 53.2148 19.9882 0001349 90.6509 269.4637 15.08836656 02
| Epoch (UTC): | 25 May 2026 09:14:48 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.9882° |
| argument of perigee: | 90.6509° |
| revolutions per day: | 15.08836656 |
| mean anomaly at epoch: | 269.4637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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