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 50205U 26145.50904229 +.00000000 +00000-0 -12023-4 0 00007
2 50205 53.2128 224.2636 0001245 86.9126 273.2009 15.08842442 05
| Epoch (UTC): | 25 May 2026 12:13:01 |
| Eccentricity: | 0.0001245 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.2636° |
| argument of perigee: | 86.9126° |
| revolutions per day: | 15.08842442 |
| mean anomaly at epoch: | 273.2009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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