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 43966U 14055V 25045.51738253 -.00000021 00000-0 00000-0 0 9997
2 43966 19.4937 182.2211 5157195 95.9599 322.3502 1.83013172 43122
| Epoch (UTC): | 14 February 2025 12:25:01 |
| Eccentricity: | 0.5157195 |
| inclination: | 19.4937° |
| perigee height: | 7294 km |
| apogee height: | 36414 km |
| right ascension of ascending node: | 182.2211° |
| argument of perigee: | 95.9599° |
| revolutions per day: | 1.83013172 |
| mean anomaly at epoch: | 322.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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