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 25196.88834528 .00004610 00000-0 19236-3 0 9997
2 19573 82.5236 354.4486 0011470 287.8753 72.1232 15.23358893983295
| Epoch (UTC): | 15 July 2025 21:19:13 |
| Eccentricity: | 0.0011470 |
| inclination: | 82.5236° |
| perigee height: | 488 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 354.4486° |
| argument of perigee: | 287.8753° |
| revolutions per day: | 15.23358893 |
| mean anomaly at epoch: | 72.1232° |
| orbit number at epoch: | 98329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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