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 58908U 24023D 24358.15559141 .00006321 00000-0 62325-3 0 9997
2 58908 49.9932 357.3835 0007230 81.6761 278.5001 14.93046731 48365
| Epoch (UTC): | 23 December 2024 03:44:03 |
| Eccentricity: | 0.0007230 |
| inclination: | 49.9932° |
| perigee height: | 583 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 357.3835° |
| argument of perigee: | 81.6761° |
| revolutions per day: | 14.93046731 |
| mean anomaly at epoch: | 278.5001° |
| orbit number at epoch: | 4836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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