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 15755U 85042A 24276.93082575 .00000390 00000-0 20141-3 0 9995
2 15755 71.1110 148.2435 0036961 233.6581 126.1132 14.20775618 38778
| Epoch (UTC): | 02 October 2024 22:20:23 |
| Eccentricity: | 0.0036961 |
| inclination: | 71.1110° |
| perigee height: | 796 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 148.2435° |
| argument of perigee: | 233.6581° |
| revolutions per day: | 14.20775618 |
| mean anomaly at epoch: | 126.1132° |
| orbit number at epoch: | 3877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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