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 40032U 26108.25108750 +.00000000 +00000-0 +29462-3 0 00003
2 40032 98.0754 101.4421 0008319 32.2605 327.9133 15.14361152 03
| Epoch (UTC): | 18 April 2026 06:01:33 |
| Eccentricity: | 0.0008319 |
| inclination: | 98.0754° |
| perigee height: | 517 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 101.4421° |
| argument of perigee: | 32.2605° |
| revolutions per day: | 15.14361152 |
| mean anomaly at epoch: | 327.9133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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