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 26145.58895484 +.00000000 +00000-0 +20371-3 0 00009
2 23439 64.8188 339.7652 0155301 8.0379 352.2982 11.27583633 05
| Epoch (UTC): | 25 May 2026 14:08:05 |
| Eccentricity: | 0.0155301 |
| inclination: | 64.8188° |
| perigee height: | 1892 km |
| apogee height: | 2153 km |
| right ascension of ascending node: | 339.7652° |
| argument of perigee: | 8.0379° |
| revolutions per day: | 11.27583633 |
| mean anomaly at epoch: | 352.2982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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