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 59588U 24077B 24357.68197905 .00016279 00000-0 17095-1 0 9999
2 59588 97.5199 23.4028 0049625 238.7070 120.9220 13.74334257 33213
| Epoch (UTC): | 22 December 2024 16:22:02 |
| Eccentricity: | 0.0049625 |
| inclination: | 97.5199° |
| perigee height: | 947 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 23.4028° |
| argument of perigee: | 238.7070° |
| revolutions per day: | 13.74334257 |
| mean anomaly at epoch: | 120.9220° |
| orbit number at epoch: | 3321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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