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 23439U 26066.47830263 +.00000000 +00000-0 +16944-3 0 00004
2 23439 64.8142 107.7101 0152583 22.4432 338.3075 11.27583924 07
| Epoch (UTC): | 07 March 2026 11:28:45 |
| Eccentricity: | 0.0152583 |
| inclination: | 64.8142° |
| perigee height: | 1894 km |
| apogee height: | 2150 km |
| right ascension of ascending node: | 107.7101° |
| argument of perigee: | 22.4432° |
| revolutions per day: | 11.27583924 |
| mean anomaly at epoch: | 338.3075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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