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 25201.20284932 .00007319 00000-0 13625-3 0 9990
2 25544 51.6337 143.4222 0002199 96.8401 263.2838 15.49966786520284
| Epoch (UTC): | 20 July 2025 04:52:06 |
| Eccentricity: | 0.0002199 |
| inclination: | 51.6337° |
| perigee height: | 415 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 143.4222° |
| argument of perigee: | 96.8401° |
| revolutions per day: | 15.49966786 |
| mean anomaly at epoch: | 263.2838° |
| orbit number at epoch: | 52028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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