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 26074.28152939 +.00000000 +00000-0 +40201-3 0 00005
2 32289 97.8270 105.0652 0001573 82.2684 277.8713 14.90395445 03
| Epoch (UTC): | 15 March 2026 06:45:24 |
| Eccentricity: | 0.0001573 |
| inclination: | 97.8270° |
| perigee height: | 596 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 105.0652° |
| argument of perigee: | 82.2684° |
| revolutions per day: | 14.90395445 |
| mean anomaly at epoch: | 277.8713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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