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 22826U 93061D 23086.87370537 .00000283 00000-0 12592-3 0 9993
2 22826 98.8468 128.2785 0007933 294.0742 65.9609 14.30629116538934
| Epoch (UTC): | 27 March 2023 20:58:08 |
| Eccentricity: | 0.0007933 |
| inclination: | 98.8468° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 128.2785° |
| argument of perigee: | 294.0742° |
| revolutions per day: | 14.30629116 |
| mean anomaly at epoch: | 65.9609° |
| orbit number at epoch: | 53893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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