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 20433U 90004B 21064.14889672 .00000004 00000-0 10240-4 0 9998
2 20433 74.0374 24.7747 0041140 184.8900 186.1864 14.36122500629993
| Epoch (UTC): | 05 March 2021 03:34:24 |
| Eccentricity: | 0.0041140 |
| inclination: | 74.0374° |
| perigee height: | 742 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 24.7747° |
| argument of perigee: | 184.8900° |
| revolutions per day: | 14.36122500 |
| mean anomaly at epoch: | 186.1864° |
| orbit number at epoch: | 62999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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