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 26072.50915844 +.00000000 +00000-0 -75323-4 0 00002
2 23439 64.8133 97.9551 0152805 21.3124 339.4075 11.27583879 00
| Epoch (UTC): | 13 March 2026 12:13:11 |
| Eccentricity: | 0.0152805 |
| inclination: | 64.8133° |
| perigee height: | 1894 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 97.9551° |
| argument of perigee: | 21.3124° |
| revolutions per day: | 11.27583879 |
| mean anomaly at epoch: | 339.4075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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