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 22176.15435863 .00000160 00000-0 00000-0 0 9997
2 44475 0.0189 261.3862 0000679 179.6663 278.9494 1.00271967 10638
| Epoch (UTC): | 25 June 2022 03:42:16 |
| Eccentricity: | 0.0000679 |
| inclination: | 0.0189° |
| perigee height: | 35783 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 261.3862° |
| argument of perigee: | 179.6663° |
| revolutions per day: | 1.00271967 |
| mean anomaly at epoch: | 278.9494° |
| orbit number at epoch: | 1063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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