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 26075.20754492 +.00000000 +00000-0 +43521-3 0 00003
2 40032 98.0728 66.4072 0009174 124.1693 236.0408 15.13800114 04
| Epoch (UTC): | 16 March 2026 04:58:51 |
| Eccentricity: | 0.0009174 |
| inclination: | 98.0728° |
| perigee height: | 518 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 66.4072° |
| argument of perigee: | 124.1693° |
| revolutions per day: | 15.13800114 |
| mean anomaly at epoch: | 236.0408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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