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 22229.17202829 .00001890 00000-0 18728-3 0 9998
2 32791 97.6161 203.5477 0012496 355.8128 4.2985 14.92926969776337
| Epoch (UTC): | 17 August 2022 04:07:43 |
| Eccentricity: | 0.0012496 |
| inclination: | 97.6161° |
| perigee height: | 580 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 203.5477° |
| argument of perigee: | 355.8128° |
| revolutions per day: | 14.92926969 |
| mean anomaly at epoch: | 4.2985° |
| orbit number at epoch: | 77633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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