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 32289U 26071.19317852 +.00000000 +00000-0 +93183-4 0 00007
2 32289 97.8278 102.0055 0001717 81.1969 278.9444 14.90377301 03
| Epoch (UTC): | 12 March 2026 04:38:10 |
| Eccentricity: | 0.0001717 |
| inclination: | 97.8278° |
| perigee height: | 596 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 102.0055° |
| argument of perigee: | 81.1969° |
| revolutions per day: | 14.90377301 |
| mean anomaly at epoch: | 278.9444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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