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 37589U 99025EKH 24356.51933526 .00006439 00000-0 38969-2 0 9990
2 37589 99.0777 252.4115 0122047 174.3483 185.9093 14.03140297775790
| Epoch (UTC): | 21 December 2024 12:27:50 |
| Eccentricity: | 0.0122047 |
| inclination: | 99.0777° |
| perigee height: | 794 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 252.4115° |
| argument of perigee: | 174.3483° |
| revolutions per day: | 14.03140297 |
| mean anomaly at epoch: | 185.9093° |
| orbit number at epoch: | 77579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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