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 19573U 88093A 23270.53459662 .00006494 00000-0 39407-3 0 9996
2 19573 82.5222 282.1542 0018122 52.9335 307.3548 15.10223095904857
| Epoch (UTC): | 27 September 2023 12:49:49 |
| Eccentricity: | 0.0018122 |
| inclination: | 82.5222° |
| perigee height: | 523 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 282.1542° |
| argument of perigee: | 52.9335° |
| revolutions per day: | 15.10223095 |
| mean anomaly at epoch: | 307.3548° |
| orbit number at epoch: | 90485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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