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 00022U 59009A 21023.51019842 .00000029 00000-0 25480-4 0 9999
2 00022 50.2834 149.3886 0138846 19.6375 340.9846 14.95387426503290
| Epoch (UTC): | 23 January 2021 12:14:41 |
| Eccentricity: | 0.0138846 |
| inclination: | 50.2834° |
| perigee height: | 484 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 149.3886° |
| argument of perigee: | 19.6375° |
| revolutions per day: | 14.95387426 |
| mean anomaly at epoch: | 340.9846° |
| orbit number at epoch: | 50329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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