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 25189.14667821 .00005417 00000-0 20803-3 0 9993
2 19274 82.4724 150.2533 0012814 324.9592 35.0802 15.26155731 18925
| Epoch (UTC): | 08 July 2025 03:31:12 |
| Eccentricity: | 0.0012814 |
| inclination: | 82.4724° |
| perigee height: | 478 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 150.2533° |
| argument of perigee: | 324.9592° |
| revolutions per day: | 15.26155731 |
| mean anomaly at epoch: | 35.0802° |
| orbit number at epoch: | 1892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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