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 19573U 88093A 25188.54595355 .00005115 00000-0 21407-3 0 9997
2 19573 82.5220 2.7604 0011855 320.4327 39.6043 15.23282322982022
| Epoch (UTC): | 07 July 2025 13:06:10 |
| Eccentricity: | 0.0011855 |
| inclination: | 82.5220° |
| perigee height: | 488 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 2.7604° |
| argument of perigee: | 320.4327° |
| revolutions per day: | 15.23282322 |
| mean anomaly at epoch: | 39.6043° |
| orbit number at epoch: | 98202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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