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 11963U 26022.31116448 +.00000000 +00000-0 +84914-4 0 00003
2 11963 81.2791 319.1625 0074207 183.9487 176.1109 14.10150894 05
| Epoch (UTC): | 22 January 2026 07:28:04 |
| Eccentricity: | 0.0074207 |
| inclination: | 81.2791° |
| perigee height: | 805 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 319.1625° |
| argument of perigee: | 183.9487° |
| revolutions per day: | 14.10150894 |
| mean anomaly at epoch: | 176.1109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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