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 19046U 88032B 22228.14150450 .00002156 00000-0 15846-3 0 9998
2 19046 97.3945 224.4654 0037112 37.3817 322.9980 15.03890368855878
| Epoch (UTC): | 16 August 2022 03:23:45 |
| Eccentricity: | 0.0037112 |
| inclination: | 97.3945° |
| perigee height: | 529 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 224.4654° |
| argument of perigee: | 37.3817° |
| revolutions per day: | 15.03890368 |
| mean anomaly at epoch: | 322.9980° |
| orbit number at epoch: | 85587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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