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 25544U 98067A 25171.80882408 .00010734 00000-0 19478-3 0 9991
2 25544 51.6358 289.1269 0002114 264.7605 95.3143 15.50148846515722
| Epoch (UTC): | 20 June 2025 19:24:42 |
| Eccentricity: | 0.0002114 |
| inclination: | 51.6358° |
| perigee height: | 415 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 289.1269° |
| argument of perigee: | 264.7605° |
| revolutions per day: | 15.50148846 |
| mean anomaly at epoch: | 95.3143° |
| orbit number at epoch: | 51572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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