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 23265.60778521 .00000046 00000-0 00000-0 0 9995
2 44071 0.0198 154.3714 0000642 313.9937 171.9436 1.00278412 16618
| Epoch (UTC): | 22 September 2023 14:35:12 |
| Eccentricity: | 0.0000642 |
| inclination: | 0.0198° |
| perigee height: | 35781 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 154.3714° |
| argument of perigee: | 313.9937° |
| revolutions per day: | 1.00278412 |
| mean anomaly at epoch: | 171.9436° |
| orbit number at epoch: | 1661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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