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 66973U 26145.46902135 +.00000000 +00000-0 +74603-3 0 00005
2 66973 42.9983 309.5188 0001389 304.3780 55.6940 15.27591183 09
| Epoch (UTC): | 25 May 2026 11:15:23 |
| Eccentricity: | 0.0001389 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.5188° |
| argument of perigee: | 304.3780° |
| revolutions per day: | 15.27591183 |
| mean anomaly at epoch: | 55.6940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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