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 15331U 84105A 22144.68192592 .00004425 00000-0 22992-3 0 9998
2 15331 82.5380 356.7624 0014119 168.9977 191.1567 15.15757022 54270
| Epoch (UTC): | 24 May 2022 16:21:58 |
| Eccentricity: | 0.0014119 |
| inclination: | 82.5380° |
| perigee height: | 509 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 356.7624° |
| argument of perigee: | 168.9977° |
| revolutions per day: | 15.15757022 |
| mean anomaly at epoch: | 191.1567° |
| orbit number at epoch: | 5427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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