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 25193.80179114 .00006494 00000-0 24931-3 0 9996
2 19274 82.4736 145.5663 0012402 306.6692 53.3406 15.26206853998427
| Epoch (UTC): | 12 July 2025 19:14:34 |
| Eccentricity: | 0.0012402 |
| inclination: | 82.4736° |
| perigee height: | 478 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 145.5663° |
| argument of perigee: | 306.6692° |
| revolutions per day: | 15.26206853 |
| mean anomaly at epoch: | 53.3406° |
| orbit number at epoch: | 99842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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