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 22139.84120767 .00002586 00000-0 19068-3 0 9991
2 19046 97.3919 140.0598 0035864 339.8392 20.1416 15.03639783842609
| Epoch (UTC): | 19 May 2022 20:11:20 |
| Eccentricity: | 0.0035864 |
| inclination: | 97.3919° |
| perigee height: | 531 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 140.0598° |
| argument of perigee: | 339.8392° |
| revolutions per day: | 15.03639783 |
| mean anomaly at epoch: | 20.1416° |
| orbit number at epoch: | 84260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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