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 15370U 84111B 24260.93986237 .00001732 00000-0 19934-3 0 9994
2 15370 82.5158 43.2069 0019458 318.6571 41.3171 14.85085418156989
| Epoch (UTC): | 16 September 2024 22:33:24 |
| Eccentricity: | 0.0019458 |
| inclination: | 82.5158° |
| perigee height: | 600 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 43.2069° |
| argument of perigee: | 318.6571° |
| revolutions per day: | 14.85085418 |
| mean anomaly at epoch: | 41.3171° |
| orbit number at epoch: | 15698 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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