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 26960U 26029.66243300 +.00000000 +00000-0 +28337-3 0 00005
2 26960 97.6336 124.2532 0009625 280.3309 79.6908 16.45653777 05
| Epoch (UTC): | 29 January 2026 15:53:54 |
| Eccentricity: | 0.0009625 |
| inclination: | 97.6336° |
| perigee height: | 145 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 124.2532° |
| argument of perigee: | 280.3309° |
| revolutions per day: | 16.45653777 |
| mean anomaly at epoch: | 79.6908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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