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 08846U 76043B 23333.60368269 .00000224 00000-0 12180-3 0 9993
2 08846 81.2254 178.5964 0037724 206.3912 153.5337 14.08753052442514
| Epoch (UTC): | 29 November 2023 14:29:18 |
| Eccentricity: | 0.0037724 |
| inclination: | 81.2254° |
| perigee height: | 836 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 178.5964° |
| argument of perigee: | 206.3912° |
| revolutions per day: | 14.08753052 |
| mean anomaly at epoch: | 153.5337° |
| orbit number at epoch: | 44251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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