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 26138.82328941 +.00000000 +00000-0 -80545-4 0 00005
2 20169 7.2789 332.4885 7192850 319.2221 4.7780 2.26412246 03
| Epoch (UTC): | 18 May 2026 19:45:32 |
| Eccentricity: | 0.7192850 |
| inclination: | 7.2789° |
| perigee height: | 499 km |
| apogee height: | 35741 km |
| right ascension of ascending node: | 332.4885° |
| argument of perigee: | 319.2221° |
| revolutions per day: | 2.26412246 |
| mean anomaly at epoch: | 4.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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