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 19210U 88050A 24277.21896818 .00016437 00000-0 81153-3 0 9991
2 19210 82.5126 319.8854 0015275 151.9238 208.2823 15.17670189979360
| Epoch (UTC): | 03 October 2024 05:15:18 |
| Eccentricity: | 0.0015275 |
| inclination: | 82.5126° |
| perigee height: | 502 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 319.8854° |
| argument of perigee: | 151.9238° |
| revolutions per day: | 15.17670189 |
| mean anomaly at epoch: | 208.2823° |
| orbit number at epoch: | 97936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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