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 10961U 26100.26866498 +.00000000 +00000-0 +64950-4 0 00006
2 10961 74.0766 213.0055 0015785 24.1480 336.0411 14.37586089 09
| Epoch (UTC): | 10 April 2026 06:26:52 |
| Eccentricity: | 0.0015785 |
| inclination: | 74.0766° |
| perigee height: | 755 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 213.0055° |
| argument of perigee: | 24.1480° |
| revolutions per day: | 14.37586089 |
| mean anomaly at epoch: | 336.0411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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