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 20066U 26139.77322281 +.00000000 +00000-0 +00000-0 0 00000
2 20066 12.9282 341.8294 0001877 292.9265 60.8827 0.98821281 09
| Epoch (UTC): | 19 May 2026 18:33:26 |
| Eccentricity: | 0.0001877 |
| inclination: | 12.9282° |
| perigee height: | 36190 km |
| apogee height: | 36206 km |
| right ascension of ascending node: | 341.8294° |
| argument of perigee: | 292.9265° |
| revolutions per day: | 0.98821281 |
| mean anomaly at epoch: | 60.8827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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