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 25544U 98067A 23269.24596594 .00022911 00000-0 41242-3 0 9997
2 25544 51.6431 187.9644 0005811 63.9094 71.6410 15.49698684417468
| Epoch (UTC): | 26 September 2023 05:54:11 |
| Eccentricity: | 0.0005811 |
| inclination: | 51.6431° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 187.9644° |
| argument of perigee: | 63.9094° |
| revolutions per day: | 15.49698684 |
| mean anomaly at epoch: | 71.6410° |
| orbit number at epoch: | 41746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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