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 50465U 21131A 24358.21647344 .00000379 00000-0 14740-3 0 9999
2 50465 98.4946 74.3199 0000350 62.3123 297.8098 14.35356361156811
| Epoch (UTC): | 23 December 2024 05:11:43 |
| Eccentricity: | 0.0000350 |
| inclination: | 98.4946° |
| perigee height: | 773 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 74.3199° |
| argument of perigee: | 62.3123° |
| revolutions per day: | 14.35356361 |
| mean anomaly at epoch: | 297.8098° |
| orbit number at epoch: | 15681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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