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 44873U 19092A 22228.88283943 .00000256 00000-0 38749-4 0 9996
2 44873 97.8890 51.6767 0001428 84.3393 275.7989 14.82160195144054
| Epoch (UTC): | 16 August 2022 21:11:17 |
| Eccentricity: | 0.0001428 |
| inclination: | 97.8890° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 51.6767° |
| argument of perigee: | 84.3393° |
| revolutions per day: | 14.82160195 |
| mean anomaly at epoch: | 275.7989° |
| orbit number at epoch: | 14405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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