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 26075.82061865 +.00000000 +00000-0 +15528-3 0 00003
2 20666 62.7822 229.5990 0025936 348.7791 11.2726 15.03630990 04
| Epoch (UTC): | 16 March 2026 19:41:41 |
| Eccentricity: | 0.0025936 |
| inclination: | 62.7822° |
| perigee height: | 538 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 229.5990° |
| argument of perigee: | 348.7791° |
| revolutions per day: | 15.03630990 |
| mean anomaly at epoch: | 11.2726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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