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 66820U 26145.33743483 +.00000000 +00000-0 +18909-3 0 00008
2 66820 97.6997 94.1070 0010373 82.9030 277.3373 15.00225537 00
| Epoch (UTC): | 25 May 2026 08:05:54 |
| Eccentricity: | 0.0010373 |
| inclination: | 97.6997° |
| perigee height: | 559 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 94.1070° |
| argument of perigee: | 82.9030° |
| revolutions per day: | 15.00225537 |
| mean anomaly at epoch: | 277.3373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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