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 57585U 23117F 24358.18362230 .00018638 00000-0 76680-3 0 9997
2 57585 97.4695 68.9440 0009422 1.6295 358.4971 15.24154488 75903
| Epoch (UTC): | 23 December 2024 04:24:24 |
| Eccentricity: | 0.0009422 |
| inclination: | 97.4695° |
| perigee height: | 487 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 68.9440° |
| argument of perigee: | 1.6295° |
| revolutions per day: | 15.24154488 |
| mean anomaly at epoch: | 358.4971° |
| orbit number at epoch: | 7590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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