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 26074U 00006D 24277.72604300 .00000472 00000-0 49937-3 0 9997
2 26074 70.9657 32.9116 0212903 45.9737 315.8683 13.69885300273727
| Epoch (UTC): | 03 October 2024 17:25:30 |
| Eccentricity: | 0.0212903 |
| inclination: | 70.9657° |
| perigee height: | 843 km |
| apogee height: | 1157 km |
| right ascension of ascending node: | 32.9116° |
| argument of perigee: | 45.9737° |
| revolutions per day: | 13.69885300 |
| mean anomaly at epoch: | 315.8683° |
| orbit number at epoch: | 27372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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