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 26135.30102123 +.00000000 +00000-0 -21749-3 0 00000
2 23439 64.8191 356.4041 0155029 9.9019 350.4902 11.27583653 09
| Epoch (UTC): | 15 May 2026 07:13:28 |
| Eccentricity: | 0.0155029 |
| inclination: | 64.8191° |
| perigee height: | 1892 km |
| apogee height: | 2153 km |
| right ascension of ascending node: | 356.4041° |
| argument of perigee: | 9.9019° |
| revolutions per day: | 11.27583653 |
| mean anomaly at epoch: | 350.4902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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