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 07735U 75027B 25193.91692592 -.00000077 00000-0 42477-4 0 9999
2 07735 114.9771 72.7197 0036896 351.4020 8.6427 14.25450393610116
| Epoch (UTC): | 12 July 2025 22:00:22 |
| Eccentricity: | 0.0036896 |
| inclination: | 114.9771° |
| perigee height: | 780 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 72.7197° |
| argument of perigee: | 351.4020° |
| revolutions per day: | 14.25450393 |
| mean anomaly at epoch: | 8.6427° |
| orbit number at epoch: | 61011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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