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 25312.42041502 .00013418 00000-0 24734-3 0 9991
2 25544 51.6332 312.3676 0004093 47.8963 312.2373 15.49452868537539
| Epoch (UTC): | 08 November 2025 10:05:23 |
| Eccentricity: | 0.0004093 |
| inclination: | 51.6332° |
| perigee height: | 415 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 312.3676° |
| argument of perigee: | 47.8963° |
| revolutions per day: | 15.49452868 |
| mean anomaly at epoch: | 312.2373° |
| orbit number at epoch: | 53753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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