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 44420U 19036AC 22320.00463817 .06035209 00000-0 44554-1 0 9999
2 44420 23.9883 192.8403 0026944 276.6165 212.0548 15.67402264179909
| Epoch (UTC): | 16 November 2022 00:06:40 |
| Eccentricity: | 0.0026944 |
| inclination: | 23.9883° |
| perigee height: | 348 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 192.8403° |
| argument of perigee: | 276.6165° |
| revolutions per day: | 15.67402264 |
| mean anomaly at epoch: | 212.0548° |
| orbit number at epoch: | 17990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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