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 50836U 26145.39034014 +.00000000 +00000-0 +94360-4 0 00003
2 50836 53.2140 194.5754 0001130 86.2679 273.8442 15.08836472 01
| Epoch (UTC): | 25 May 2026 09:22:05 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.5754° |
| argument of perigee: | 86.2679° |
| revolutions per day: | 15.08836472 |
| mean anomaly at epoch: | 273.8442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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