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 26150.54142611 +.00000000 +00000-0 +48767-3 0 00000
2 32289 97.8158 180.5939 0001764 97.3834 262.7584 14.90707469 02
| Epoch (UTC): | 30 May 2026 12:59:39 |
| Eccentricity: | 0.0001764 |
| inclination: | 97.8158° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 180.5939° |
| argument of perigee: | 97.3834° |
| revolutions per day: | 14.90707469 |
| mean anomaly at epoch: | 262.7584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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