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 09661U 26088.22391310 +.00000000 +00000-0 +21389-4 0 00007
2 09661 81.2675 170.9043 0009947 209.4779 150.5829 14.04212738 06
| Epoch (UTC): | 29 March 2026 05:22:26 |
| Eccentricity: | 0.0009947 |
| inclination: | 81.2675° |
| perigee height: | 872 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 170.9043° |
| argument of perigee: | 209.4779° |
| revolutions per day: | 14.04212738 |
| mean anomaly at epoch: | 150.5829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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