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 26073.30735987 +.00000000 +00000-0 +27269-5 0 00005
2 23439 64.8133 96.6641 0152831 21.1629 339.5528 11.27583899 09
| Epoch (UTC): | 14 March 2026 07:22:35 |
| Eccentricity: | 0.0152831 |
| inclination: | 64.8133° |
| perigee height: | 1894 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 96.6641° |
| argument of perigee: | 21.1629° |
| revolutions per day: | 11.27583899 |
| mean anomaly at epoch: | 339.5528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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