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 20478U 26129.78686780 +.00000000 +00000-0 -19681-4 0 00004
2 20478 99.2207 190.8570 0004471 293.3877 66.6814 13.96062117 04
| Epoch (UTC): | 09 May 2026 18:53:05 |
| Eccentricity: | 0.0004471 |
| inclination: | 99.2207° |
| perigee height: | 904 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 190.8570° |
| argument of perigee: | 293.3877° |
| revolutions per day: | 13.96062117 |
| mean anomaly at epoch: | 66.6814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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