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 19822U 89016A 22225.89004139 .00053387 28267-6 79070-3 0 9996
2 19822 74.9906 148.1229 1488414 94.0616 283.1328 12.62648142136386
| Epoch (UTC): | 13 August 2022 21:21:39 |
| Eccentricity: | 0.1488414 |
| inclination: | 74.9906° |
| perigee height: | 252 km |
| apogee height: | 2571 km |
| right ascension of ascending node: | 148.1229° |
| argument of perigee: | 94.0616° |
| revolutions per day: | 12.62648142 |
| mean anomaly at epoch: | 283.1328° |
| orbit number at epoch: | 13638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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