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 24279.46943132 .00032942 00000-0 59769-3 0 9995
2 25544 51.6363 129.1425 0009147 39.7917 320.3740 15.49242162475659
| Epoch (UTC): | 05 October 2024 11:15:58 |
| Eccentricity: | 0.0009147 |
| inclination: | 51.6363° |
| perigee height: | 413 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 129.1425° |
| argument of perigee: | 39.7917° |
| revolutions per day: | 15.49242162 |
| mean anomaly at epoch: | 320.3740° |
| orbit number at epoch: | 47565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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