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 10521U 77119B 23150.86272159 .00000246 00000-0 84244-4 0 9993
2 10521 74.0265 203.2931 0020116 43.2680 317.0051 14.41172753385006
| Epoch (UTC): | 30 May 2023 20:42:19 |
| Eccentricity: | 0.0020116 |
| inclination: | 74.0265° |
| perigee height: | 740 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 203.2931° |
| argument of perigee: | 43.2680° |
| revolutions per day: | 14.41172753 |
| mean anomaly at epoch: | 317.0051° |
| orbit number at epoch: | 38500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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