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 23344.80043927 .00000248 00000-0 84666-4 0 9991
2 10521 74.0257 204.0247 0020815 356.4597 3.6408 14.41352315413255
| Epoch (UTC): | 10 December 2023 19:12:37 |
| Eccentricity: | 0.0020815 |
| inclination: | 74.0257° |
| perigee height: | 739 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 204.0247° |
| argument of perigee: | 356.4597° |
| revolutions per day: | 14.41352315 |
| mean anomaly at epoch: | 3.6408° |
| orbit number at epoch: | 41325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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