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 44354U 19036R 22176.17660390 .00068567 -49052-5 60171-3 0 9995
2 44354 28.5230 124.7802 0226611 57.7295 304.5049 15.40806814165867
| Epoch (UTC): | 25 June 2022 04:14:18 |
| Eccentricity: | 0.0226611 |
| inclination: | 28.5230° |
| perigee height: | 289 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 124.7802° |
| argument of perigee: | 57.7295° |
| revolutions per day: | 15.40806814 |
| mean anomaly at epoch: | 304.5049° |
| orbit number at epoch: | 16586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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