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 26069.50270737 +.00000000 +00000-0 +20406-3 0 00002
2 20666 62.7824 251.0854 0024843 347.1642 12.8822 15.03599210 02
| Epoch (UTC): | 10 March 2026 12:03:53 |
| Eccentricity: | 0.0024843 |
| inclination: | 62.7824° |
| perigee height: | 539 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 251.0854° |
| argument of perigee: | 347.1642° |
| revolutions per day: | 15.03599210 |
| mean anomaly at epoch: | 12.8822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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