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 22228.87339823 .00002142 00000-0 15750-3 0 9990
2 19046 97.3947 225.1653 0037070 34.9832 325.3819 15.03893612855693
| Epoch (UTC): | 16 August 2022 20:57:41 |
| Eccentricity: | 0.0037070 |
| inclination: | 97.3947° |
| perigee height: | 529 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 225.1653° |
| argument of perigee: | 34.9832° |
| revolutions per day: | 15.03893612 |
| mean anomaly at epoch: | 325.3819° |
| orbit number at epoch: | 85569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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