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 50193U 26145.28453036 +.00000000 +00000-0 +49964-4 0 00006
2 50193 53.2148 255.2721 0001135 89.4539 270.6584 15.08835683 04
| Epoch (UTC): | 25 May 2026 06:49:43 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 255.2721° |
| argument of perigee: | 89.4539° |
| revolutions per day: | 15.08835683 |
| mean anomaly at epoch: | 270.6584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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