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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 19460U 88078A 25088.85233213 .00000459 00000-0 15663-3 0 9993
2 19460 84.9912 11.3722 0005021 89.7650 270.4119 14.34252063 45490
| Epoch (UTC): | 29 March 2025 20:27:21 |
| Eccentricity: | 0.0005021 |
| inclination: | 84.9912° |
| perigee height: | 774 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 11.3722° |
| argument of perigee: | 89.7650° |
| revolutions per day: | 14.34252063 |
| mean anomaly at epoch: | 270.4119° |
| orbit number at epoch: | 4549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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