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 58992U 24034A 25167.20210178 .00003007 00000-0 24678-3 0 9998
2 58992 98.2422 165.2888 0034981 286.2743 73.4632 14.99617137 72324
| Epoch (UTC): | 16 June 2025 04:51:01 |
| Eccentricity: | 0.0034981 |
| inclination: | 98.2422° |
| perigee height: | 544 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 165.2888° |
| argument of perigee: | 286.2743° |
| revolutions per day: | 14.99617137 |
| mean anomaly at epoch: | 73.4632° |
| orbit number at epoch: | 7232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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