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 data is extracted from the following two-line orbital elements,
1 43188U 18014J 23338.22377171 .00005024 00000-0 38626-3 0 9996
2 43188 97.6011 238.7266 0011877 313.4272 46.5963 15.02104615319067
| Epoch (UTC): | 04 December 2023 05:22:13 |
| Eccentricity: | 0.0011877 |
| inclination: | 97.6011° |
| perigee height: | 552 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 238.7266° |
| argument of perigee: | 313.4272° |
| revolutions per day: | 15.02104615 |
| mean anomaly at epoch: | 46.5963° |
| orbit number at epoch: | 31906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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