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 25194.17630689 .00009469 00000-0 17059-3 0 9994
2 25544 51.6340 178.2487 0002656 5.9347 354.1673 15.50514308519191
| Epoch (UTC): | 13 July 2025 04:13:52 |
| Eccentricity: | 0.0002656 |
| inclination: | 51.6340° |
| perigee height: | 413 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 178.2487° |
| argument of perigee: | 5.9347° |
| revolutions per day: | 15.50514308 |
| mean anomaly at epoch: | 354.1673° |
| orbit number at epoch: | 51919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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