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 32382U 26150.61506549 +.00000000 +00000-0 +80197-4 0 00000
2 32382 98.5775 157.7983 0001297 86.1355 273.9975 14.29984528 02
| Epoch (UTC): | 30 May 2026 14:45:41 |
| Eccentricity: | 0.0001297 |
| inclination: | 98.5775° |
| perigee height: | 791 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 157.7983° |
| argument of perigee: | 86.1355° |
| revolutions per day: | 14.29984528 |
| mean anomaly at epoch: | 273.9975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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