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 26071.99883845 +.00000000 +00000-0 +19179-3 0 00007
2 32289 97.8278 102.8032 0001652 80.3514 279.7890 14.90381072 05
| Epoch (UTC): | 12 March 2026 23:58:19 |
| Eccentricity: | 0.0001652 |
| inclination: | 97.8278° |
| perigee height: | 596 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 102.8032° |
| argument of perigee: | 80.3514° |
| revolutions per day: | 14.90381072 |
| mean anomaly at epoch: | 279.7890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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