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 25167.63573752 .00011754 00000-0 21179-3 0 9990
2 25544 51.6388 309.8053 0000950 248.3368 207.3878 15.50244021515076
| Epoch (UTC): | 16 June 2025 15:15:27 |
| Eccentricity: | 0.0000950 |
| inclination: | 51.6388° |
| perigee height: | 415 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 309.8053° |
| argument of perigee: | 248.3368° |
| revolutions per day: | 15.50244021 |
| mean anomaly at epoch: | 207.3878° |
| orbit number at epoch: | 51507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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