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 32790U 26106.67096299 +.00000000 +00000-0 +17740-3 0 00009
2 32790 97.8613 85.2900 0008645 248.4961 111.5344 15.05178716 08
| Epoch (UTC): | 16 April 2026 16:06:11 |
| Eccentricity: | 0.0008645 |
| inclination: | 97.8613° |
| perigee height: | 545 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 85.2900° |
| argument of perigee: | 248.4961° |
| revolutions per day: | 15.05178716 |
| mean anomaly at epoch: | 111.5344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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