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 23086.20188432 .00024982 00000-0 45015-3 0 9990
2 25544 51.6429 14.7356 0005804 135.3885 8.0988 15.49616489389078
| Epoch (UTC): | 27 March 2023 04:50:42 |
| Eccentricity: | 0.0005804 |
| inclination: | 51.6429° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 14.7356° |
| argument of perigee: | 135.3885° |
| revolutions per day: | 15.49616489 |
| mean anomaly at epoch: | 8.0988° |
| orbit number at epoch: | 38907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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