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 50850U 26145.44461076 +.00000000 +00000-0 +34333-3 0 00000
2 50850 53.2110 154.5536 0001109 72.2629 287.8484 15.08811693 03
| Epoch (UTC): | 25 May 2026 10:40:14 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.2110° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.5536° |
| argument of perigee: | 72.2629° |
| revolutions per day: | 15.08811693 |
| mean anomaly at epoch: | 287.8484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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