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 20217U 26053.44489097 +.00000000 +00000-0 +00000-0 0 00006
2 20217 14.8500 347.6462 0043101 144.0861 64.7521 0.97410803 04
| Epoch (UTC): | 22 February 2026 10:40:38 |
| Eccentricity: | 0.0043101 |
| inclination: | 14.8500° |
| perigee height: | 36423 km |
| apogee height: | 36793 km |
| right ascension of ascending node: | 347.6462° |
| argument of perigee: | 144.0861° |
| revolutions per day: | 0.97410803 |
| mean anomaly at epoch: | 64.7521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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