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 43114U 18004D 24038.27551656 .13497234 24779-5 33124-3 0 9993
2 43114 97.2709 127.4987 0010196 278.9696 81.0452 16.45388721338886
| Epoch (UTC): | 07 February 2024 06:36:44 |
| Eccentricity: | 0.0010196 |
| inclination: | 97.2709° |
| perigee height: | 145 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 127.4987° |
| argument of perigee: | 278.9696° |
| revolutions per day: | 16.45388721 |
| mean anomaly at epoch: | 81.0452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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