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 7735U 75027B 25194.47819122 -.00000075 00000-0 43551-4 0 9993
2 7735 114.9770 74.2753 0036957 351.2166 8.8266 14.25450519610255
| Epoch (UTC): | 13 July 2025 11:28:35 |
| Eccentricity: | 0.0036957 |
| inclination: | 114.9770° |
| perigee height: | 780 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 74.2753° |
| argument of perigee: | 351.2166° |
| revolutions per day: | 14.25450519 |
| mean anomaly at epoch: | 8.8266° |
| orbit number at epoch: | 61025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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