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 25732U 99025C 23147.13511134 .00000064 00000-0 52855-4 0 9999
2 25732 98.8048 191.5709 0037738 26.3101 36.1292 14.17822060244094
| Epoch (UTC): | 27 May 2023 03:14:33 |
| Eccentricity: | 0.0037738 |
| inclination: | 98.8048° |
| perigee height: | 805 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 191.5709° |
| argument of perigee: | 26.3101° |
| revolutions per day: | 14.17822060 |
| mean anomaly at epoch: | 36.1292° |
| orbit number at epoch: | 24409 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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