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 66207U 26145.58335647 +.00000000 +00000-0 +64808-3 0 00002
2 66207 53.1588 232.9141 0001381 69.6939 133.1278 15.34389113 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001381 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 232.9141° |
| argument of perigee: | 69.6939° |
| revolutions per day: | 15.34389113 |
| mean anomaly at epoch: | 133.1278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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