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 10793U 26088.22747838 +.00000000 +00000-0 +45514-3 0 00000
2 10793 28.2302 57.7791 0874023 359.3417 0.5960 13.07580859 07
| Epoch (UTC): | 29 March 2026 05:27:34 |
| Eccentricity: | 0.0874023 |
| inclination: | 28.2302° |
| perigee height: | 567 km |
| apogee height: | 1898 km |
| right ascension of ascending node: | 57.7791° |
| argument of perigee: | 359.3417° |
| revolutions per day: | 13.07580859 |
| mean anomaly at epoch: | 0.5960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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