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 19120U 88039B 24261.05709310 .00000068 00000-0 55080-4 0 9997
2 19120 71.0137 127.3685 0019658 85.7769 274.5602 14.19452897882214
| Epoch (UTC): | 17 September 2024 01:22:12 |
| Eccentricity: | 0.0019658 |
| inclination: | 71.0137° |
| perigee height: | 813 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 127.3685° |
| argument of perigee: | 85.7769° |
| revolutions per day: | 14.19452897 |
| mean anomaly at epoch: | 274.5602° |
| orbit number at epoch: | 88221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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