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 25316.93497624 .00019039 00000-0 34560-3 0 9994
2 25544 51.6332 290.0154 0004116 64.1640 295.9773 15.49593679538237
| Epoch (UTC): | 12 November 2025 22:26:21 |
| Eccentricity: | 0.0004116 |
| inclination: | 51.6332° |
| perigee height: | 415 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 290.0154° |
| argument of perigee: | 64.1640° |
| revolutions per day: | 15.49593679 |
| mean anomaly at epoch: | 295.9773° |
| orbit number at epoch: | 53823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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