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 58202U 23168D 24358.01989157 .00028062 00000-0 21210-2 0 9995
2 58202 97.8159 5.5696 0003723 21.7077 338.4304 15.02314900 62365
| Epoch (UTC): | 23 December 2024 00:28:38 |
| Eccentricity: | 0.0003723 |
| inclination: | 97.8159° |
| perigee height: | 557 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 5.5696° |
| argument of perigee: | 21.7077° |
| revolutions per day: | 15.02314900 |
| mean anomaly at epoch: | 338.4304° |
| orbit number at epoch: | 6236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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