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 21363U 75052CH 24357.87260885 .00000294 00000-0 88171-3 0 9992
2 21363 99.6996 311.5827 0175391 86.4148 292.3744 13.10155048605560
| Epoch (UTC): | 22 December 2024 20:56:33 |
| Eccentricity: | 0.0175391 |
| inclination: | 99.6996° |
| perigee height: | 1089 km |
| apogee height: | 1356 km |
| right ascension of ascending node: | 311.5827° |
| argument of perigee: | 86.4148° |
| revolutions per day: | 13.10155048 |
| mean anomaly at epoch: | 292.3744° |
| orbit number at epoch: | 60556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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