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 32790U 26162.90496404 +.00000000 +00000-0 +25195-3 0 00002
2 32790 97.8618 142.5795 0011652 66.0447 294.1998 15.05574034 03
| Epoch (UTC): | 11 June 2026 21:43:08 |
| Eccentricity: | 0.0011652 |
| inclination: | 97.8618° |
| perigee height: | 542 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 142.5795° |
| argument of perigee: | 66.0447° |
| revolutions per day: | 15.05574034 |
| mean anomaly at epoch: | 294.1998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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