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 22146.09656027 .00002080 00000-0 15418-3 0 9993
2 19046 97.3899 146.0371 0035600 317.1847 42.6608 15.03668248843547
| Epoch (UTC): | 26 May 2022 02:19:02 |
| Eccentricity: | 0.0035600 |
| inclination: | 97.3899° |
| perigee height: | 531 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 146.0371° |
| argument of perigee: | 317.1847° |
| revolutions per day: | 15.03668248 |
| mean anomaly at epoch: | 42.6608° |
| orbit number at epoch: | 84354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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