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 62032U 26145.47591507 +.00000000 +00000-0 +47270-3 0 00005
2 62032 43.0019 182.2852 0001508 270.7067 89.3611 15.27597491 01
| Epoch (UTC): | 25 May 2026 11:25:19 |
| Eccentricity: | 0.0001508 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.2852° |
| argument of perigee: | 270.7067° |
| revolutions per day: | 15.27597491 |
| mean anomaly at epoch: | 89.3611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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