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 50842U 26145.51453132 +.00000000 +00000-0 -90977-5 0 00002
2 50842 53.2098 194.2367 0001322 81.9918 278.1224 15.08836330 07
| Epoch (UTC): | 25 May 2026 12:20:55 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.2098° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.2367° |
| argument of perigee: | 81.9918° |
| revolutions per day: | 15.08836330 |
| mean anomaly at epoch: | 278.1224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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