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 32791U 08021J 24251.97851338 .00029803 00000-0 20132-2 0 9993
2 32791 97.6990 222.8486 0007040 55.0746 305.1141 15.06507182889054
| Epoch (UTC): | 07 September 2024 23:29:03 |
| Eccentricity: | 0.0007040 |
| inclination: | 97.6990° |
| perigee height: | 542 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 222.8486° |
| argument of perigee: | 55.0746° |
| revolutions per day: | 15.06507182 |
| mean anomaly at epoch: | 305.1141° |
| orbit number at epoch: | 88905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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