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 66643U 26145.26344366 +.00000000 +00000-0 +97709-3 0 00005
2 66643 53.1592 142.6089 0000948 62.5586 297.5513 15.34411074 07
| Epoch (UTC): | 25 May 2026 06:19:21 |
| Eccentricity: | 0.0000948 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 142.6089° |
| argument of perigee: | 62.5586° |
| revolutions per day: | 15.34411074 |
| mean anomaly at epoch: | 297.5513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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