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 25197.42452828 .00006573 00000-0 12064-3 0 9996
2 25544 51.6363 162.1382 0002825 24.9428 118.6020 15.50569998519690
| Epoch (UTC): | 16 July 2025 10:11:19 |
| Eccentricity: | 0.0002825 |
| inclination: | 51.6363° |
| perigee height: | 413 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 162.1382° |
| argument of perigee: | 24.9428° |
| revolutions per day: | 15.50569998 |
| mean anomaly at epoch: | 118.6020° |
| orbit number at epoch: | 51969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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