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 36263U 99025DWQ 24357.05339889 .00010995 00000-0 34934-2 0 9990
2 36263 99.0276 211.7382 0039289 238.5518 121.1825 14.39661448828567
| Epoch (UTC): | 22 December 2024 01:16:53 |
| Eccentricity: | 0.0039289 |
| inclination: | 99.0276° |
| perigee height: | 731 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 211.7382° |
| argument of perigee: | 238.5518° |
| revolutions per day: | 14.39661448 |
| mean anomaly at epoch: | 121.1825° |
| orbit number at epoch: | 82856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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