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 19119U 88039A 25162.86411846 .00000260 00000-0 15663-3 0 9995
2 19119 71.0030 95.2370 0013208 295.3595 120.8436 14.15663312914484
| Epoch (UTC): | 11 June 2025 20:44:19 |
| Eccentricity: | 0.0013208 |
| inclination: | 71.0030° |
| perigee height: | 830 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 95.2370° |
| argument of perigee: | 295.3595° |
| revolutions per day: | 14.15663312 |
| mean anomaly at epoch: | 120.8436° |
| orbit number at epoch: | 91448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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