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 15032U 84056B 22148.78488537 .00000204 00000-0 80830-4 0 9990
2 15032 74.0718 13.1743 0016452 79.0267 281.2735 14.34910567986021
| Epoch (UTC): | 28 May 2022 18:50:14 |
| Eccentricity: | 0.0016452 |
| inclination: | 74.0718° |
| perigee height: | 763 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 13.1743° |
| argument of perigee: | 79.0267° |
| revolutions per day: | 14.34910567 |
| mean anomaly at epoch: | 281.2735° |
| orbit number at epoch: | 98602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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