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 66437U 26144.89164322 +.00000000 +00000-0 +45397-3 0 00002
2 66437 43.0033 204.1509 0002617 267.8167 92.2384 15.27590774 00
| Epoch (UTC): | 24 May 2026 21:23:57 |
| Eccentricity: | 0.0002617 |
| inclination: | 43.0033° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 204.1509° |
| argument of perigee: | 267.8167° |
| revolutions per day: | 15.27590774 |
| mean anomaly at epoch: | 92.2384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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