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 43155U 18008A 23276.51805605 .00033363 00000-0 11308-2 0 9998
2 43155 97.2846 326.6992 0009948 284.6938 75.3200 15.30435175315193
| Epoch (UTC): | 03 October 2023 12:26:00 |
| Eccentricity: | 0.0009948 |
| inclination: | 97.2846° |
| perigee height: | 468 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 326.6992° |
| argument of perigee: | 284.6938° |
| revolutions per day: | 15.30435175 |
| mean anomaly at epoch: | 75.3200° |
| orbit number at epoch: | 31519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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