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 61555U 24185D 24358.17059917 .00001897 00000-0 81157-3 0 9993
2 61555 88.9904 118.4042 0008898 18.0821 342.0686 14.24562533 19582
| Epoch (UTC): | 23 December 2024 04:05:39 |
| Eccentricity: | 0.0008898 |
| inclination: | 88.9904° |
| perigee height: | 803 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 118.4042° |
| argument of perigee: | 18.0821° |
| revolutions per day: | 14.24562533 |
| mean anomaly at epoch: | 342.0686° |
| orbit number at epoch: | 1958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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