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 8800U 76032B 24277.16325683 .00000429 00000-0 22467-3 0 9999
2 8800 81.2503 144.2937 0093772 198.1900 161.5911 14.10468326493783
| Epoch (UTC): | 03 October 2024 03:55:05 |
| Eccentricity: | 0.0093772 |
| inclination: | 81.2503° |
| perigee height: | 790 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 144.2937° |
| argument of perigee: | 198.1900° |
| revolutions per day: | 14.10468326 |
| mean anomaly at epoch: | 161.5911° |
| orbit number at epoch: | 49378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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