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 20466U 26039.14506132 +.00000000 +00000-0 +62824-4 0 00009
2 20466 82.5029 295.1416 0020851 40.6411 319.6355 14.83542898 00
| Epoch (UTC): | 08 February 2026 03:28:53 |
| Eccentricity: | 0.0020851 |
| inclination: | 82.5029° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 295.1416° |
| argument of perigee: | 40.6411° |
| revolutions per day: | 14.83542898 |
| mean anomaly at epoch: | 319.6355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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