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 44071U 19014A 21015.76855066 .00000040 00000-0 00000-0 0 9997
2 44071 0.0729 97.5536 0000499 330.4884 24.3431 1.00272256 6809
| Epoch (UTC): | 15 January 2021 18:26:42 |
| Eccentricity: | 0.0000499 |
| inclination: | 0.0729° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 97.5536° |
| argument of perigee: | 330.4884° |
| revolutions per day: | 1.00272256 |
| mean anomaly at epoch: | 24.3431° |
| orbit number at epoch: | 680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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