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 15752U 85041B 23150.92446655 .00000171 00000-0 16797-3 0 9992
2 15752 82.9477 143.0576 0023437 201.5185 158.4987 13.73189623903924
| Epoch (UTC): | 30 May 2023 22:11:13 |
| Eccentricity: | 0.0023437 |
| inclination: | 82.9477° |
| perigee height: | 971 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 143.0576° |
| argument of perigee: | 201.5185° |
| revolutions per day: | 13.73189623 |
| mean anomaly at epoch: | 158.4987° |
| orbit number at epoch: | 90392 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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