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 20465U 26100.22675220 +.00000000 +00000-0 +21275-3 0 00005
2 20465 82.4724 16.3563 0008682 218.0737 141.9881 15.11636765 05
| Epoch (UTC): | 10 April 2026 05:26:31 |
| Eccentricity: | 0.0008682 |
| inclination: | 82.4724° |
| perigee height: | 525 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 16.3563° |
| argument of perigee: | 218.0737° |
| revolutions per day: | 15.11636765 |
| mean anomaly at epoch: | 141.9881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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