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 43132U 18004X 23274.90669177 .16535587 25409-5 24982-3 0 9992
2 43132 97.2902 3.7671 0010678 260.9850 99.0246 16.48076850319334
| Epoch (UTC): | 01 October 2023 21:45:38 |
| Eccentricity: | 0.0010678 |
| inclination: | 97.2902° |
| perigee height: | 137 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 3.7671° |
| argument of perigee: | 260.9850° |
| revolutions per day: | 16.48076850 |
| mean anomaly at epoch: | 99.0246° |
| orbit number at epoch: | 31933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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