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 06659U 26088.16250191 +.00000000 +00000-0 +21407-4 0 00006
2 06659 81.1899 324.5325 0026328 272.8478 86.9679 14.10536298 01
| Epoch (UTC): | 29 March 2026 03:54:00 |
| Eccentricity: | 0.0026328 |
| inclination: | 81.1899° |
| perigee height: | 838 km |
| apogee height: | 877 km |
| right ascension of ascending node: | 324.5325° |
| argument of perigee: | 272.8478° |
| revolutions per day: | 14.10536298 |
| mean anomaly at epoch: | 86.9679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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