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 26073.48473802 +.00000000 +00000-0 -11919-3 0 00003
2 23439 64.8133 96.3771 0152840 21.1292 339.5856 11.27583869 07
| Epoch (UTC): | 14 March 2026 11:38:01 |
| Eccentricity: | 0.0152840 |
| inclination: | 64.8133° |
| perigee height: | 1894 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 96.3771° |
| argument of perigee: | 21.1292° |
| revolutions per day: | 11.27583869 |
| mean anomaly at epoch: | 339.5856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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