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 01291U 26088.16045770 +.00000000 +00000-0 +62733-4 0 00005
2 01291 70.0799 46.3988 0023225 230.7251 129.1795 13.94965391 03
| Epoch (UTC): | 29 March 2026 03:51:03 |
| Eccentricity: | 0.0023225 |
| inclination: | 70.0799° |
| perigee height: | 894 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 46.3988° |
| argument of perigee: | 230.7251° |
| revolutions per day: | 13.94965391 |
| mean anomaly at epoch: | 129.1795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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