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 19274U 88056A 25194.58855431 .00006431 00000-0 24680-3 0 9997
2 19274 82.4738 144.7741 0012339 303.4951 56.5107 15.26217259998547
| Epoch (UTC): | 13 July 2025 14:07:31 |
| Eccentricity: | 0.0012339 |
| inclination: | 82.4738° |
| perigee height: | 478 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 144.7741° |
| argument of perigee: | 303.4951° |
| revolutions per day: | 15.26217259 |
| mean anomaly at epoch: | 56.5107° |
| orbit number at epoch: | 99854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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