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 20169U 26085.83178080 +.00000000 +00000-0 +50283-3 0 00008
2 20169 7.3948 351.1979 7189386 280.8221 12.2551 2.26412575 01
| Epoch (UTC): | 26 March 2026 19:57:45 |
| Eccentricity: | 0.7189386 |
| inclination: | 7.3948° |
| perigee height: | 507 km |
| apogee height: | 35733 km |
| right ascension of ascending node: | 351.1979° |
| argument of perigee: | 280.8221° |
| revolutions per day: | 2.26412575 |
| mean anomaly at epoch: | 12.2551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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