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 18821U 88005B 24358.18059731 .00000042 00000-0 23880-4 0 9998
2 18821 82.5429 36.2724 0014608 169.7085 190.4378 13.85194782865415
| Epoch (UTC): | 23 December 2024 04:20:03 |
| Eccentricity: | 0.0014608 |
| inclination: | 82.5429° |
| perigee height: | 935 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 36.2724° |
| argument of perigee: | 169.7085° |
| revolutions per day: | 13.85194782 |
| mean anomaly at epoch: | 190.4378° |
| orbit number at epoch: | 86541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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