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 20666U 26039.30780617 +.00000000 +00000-0 +24335-3 0 00005
2 20666 62.7850 353.7555 0020360 338.6124 21.4122 15.03438946 06
| Epoch (UTC): | 08 February 2026 07:23:14 |
| Eccentricity: | 0.0020360 |
| inclination: | 62.7850° |
| perigee height: | 542 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 353.7555° |
| argument of perigee: | 338.6124° |
| revolutions per day: | 15.03438946 |
| mean anomaly at epoch: | 21.4122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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