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 25317.19293592 .00019765 00000-0 35825-3 0 9992
2 25544 51.6333 288.7385 0004163 64.5254 295.6165 15.49608679538278
| Epoch (UTC): | 13 November 2025 04:37:49 |
| Eccentricity: | 0.0004163 |
| inclination: | 51.6333° |
| perigee height: | 415 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 288.7385° |
| argument of perigee: | 64.5254° |
| revolutions per day: | 15.49608679 |
| mean anomaly at epoch: | 295.6165° |
| orbit number at epoch: | 53827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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