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 54193U 26145.63643119 +.00000000 +00000-0 +26623-4 0 00009
2 54193 53.2097 8.7349 0001172 81.2329 278.8795 15.08835513 02
| Epoch (UTC): | 25 May 2026 15:16:27 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.2097° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 8.7349° |
| argument of perigee: | 81.2329° |
| revolutions per day: | 15.08835513 |
| mean anomaly at epoch: | 278.8795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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