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 26106.53310874 +.00000000 +00000-0 +25912-3 0 00000
2 40032 98.0750 99.6195 0008468 37.3744 322.8073 15.14345462 03
| Epoch (UTC): | 16 April 2026 12:47:40 |
| Eccentricity: | 0.0008468 |
| inclination: | 98.0750° |
| perigee height: | 517 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 99.6195° |
| argument of perigee: | 37.3744° |
| revolutions per day: | 15.14345462 |
| mean anomaly at epoch: | 322.8073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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