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 26071.50585005 +.00000000 +00000-0 +52853-3 0 00002
2 40032 98.0737 62.4857 0008898 134.3660 225.8300 15.13730731 04
| Epoch (UTC): | 12 March 2026 12:08:25 |
| Eccentricity: | 0.0008898 |
| inclination: | 98.0737° |
| perigee height: | 519 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 62.4857° |
| argument of perigee: | 134.3660° |
| revolutions per day: | 15.13730731 |
| mean anomaly at epoch: | 225.8300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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