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 26077U 00006G 23333.21074854 .00000274 00000-0 29579-3 0 9991
2 26077 70.9679 196.0902 0204013 22.8729 89.2418 13.72914170193199
| Epoch (UTC): | 29 November 2023 05:03:28 |
| Eccentricity: | 0.0204013 |
| inclination: | 70.9679° |
| perigee height: | 839 km |
| apogee height: | 1139 km |
| right ascension of ascending node: | 196.0902° |
| argument of perigee: | 22.8729° |
| revolutions per day: | 13.72914170 |
| mean anomaly at epoch: | 89.2418° |
| orbit number at epoch: | 19319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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