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 10114U 77057B 25198.87934604 .00007174 00000-0 18692-3 0 9997
2 10114 97.5576 357.0525 0009451 56.1130 304.1012 15.39145855632143
| Epoch (UTC): | 17 July 2025 21:06:15 |
| Eccentricity: | 0.0009451 |
| inclination: | 97.5576° |
| perigee height: | 442 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 357.0525° |
| argument of perigee: | 56.1130° |
| revolutions per day: | 15.39145855 |
| mean anomaly at epoch: | 304.1012° |
| orbit number at epoch: | 63214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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