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 26105.83455955 +.00000000 +00000-0 +12642-3 0 00003
2 32289 97.8219 136.3222 0001326 90.7013 269.4357 14.90544052 03
| Epoch (UTC): | 15 April 2026 20:01:45 |
| Eccentricity: | 0.0001326 |
| inclination: | 97.8219° |
| perigee height: | 595 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 136.3222° |
| argument of perigee: | 90.7013° |
| revolutions per day: | 14.90544052 |
| mean anomaly at epoch: | 269.4357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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