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 39222U 26138.55057713 +.00000000 +00000-0 +00000-0 0 00004
2 39222 0.0166 319.3291 0000313 286.6447 53.2763 1.00269037 09
| Epoch (UTC): | 18 May 2026 13:12:49 |
| Eccentricity: | 0.0000313 |
| inclination: | 0.0166° |
| perigee height: | 35786 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 319.3291° |
| argument of perigee: | 286.6447° |
| revolutions per day: | 1.00269037 |
| mean anomaly at epoch: | 53.2763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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