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 44475U 19049A 22266.90580489 .00000152 00000-0 00000-0 0 9996
2 44475 0.0679 260.0102 0000943 274.5007 185.5072 1.00269021 11539
| Epoch (UTC): | 23 September 2022 21:44:21 |
| Eccentricity: | 0.0000943 |
| inclination: | 0.0679° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 260.0102° |
| argument of perigee: | 274.5007° |
| revolutions per day: | 1.00269021 |
| mean anomaly at epoch: | 185.5072° |
| orbit number at epoch: | 1153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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