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 26038.64268344 +.00000000 +00000-0 +26867-3 0 00001
2 20666 62.7851 356.0166 0020274 338.3884 21.6357 15.03435258 00
| Epoch (UTC): | 07 February 2026 15:25:27 |
| Eccentricity: | 0.0020274 |
| inclination: | 62.7851° |
| perigee height: | 542 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 356.0166° |
| argument of perigee: | 338.3884° |
| revolutions per day: | 15.03435258 |
| mean anomaly at epoch: | 21.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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