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 25166.90950966 .00008572 00000-0 15677-3 0 9995
2 25544 51.6368 313.4089 0001513 253.5073 106.5750 15.50222697514962
| Epoch (UTC): | 15 June 2025 21:49:41 |
| Eccentricity: | 0.0001513 |
| inclination: | 51.6368° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 313.4089° |
| argument of perigee: | 253.5073° |
| revolutions per day: | 15.50222697 |
| mean anomaly at epoch: | 106.5750° |
| orbit number at epoch: | 51496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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