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 26066.56699169 +.00000000 +00000-0 +11785-3 0 00000
2 23439 64.8142 107.5666 0152587 22.4265 338.3238 11.27583921 07
| Epoch (UTC): | 07 March 2026 13:36:28 |
| Eccentricity: | 0.0152587 |
| inclination: | 64.8142° |
| perigee height: | 1894 km |
| apogee height: | 2150 km |
| right ascension of ascending node: | 107.5666° |
| argument of perigee: | 22.4265° |
| revolutions per day: | 11.27583921 |
| mean anomaly at epoch: | 338.3238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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