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 44475U 19049A 23160.19866345 .00000153 00000-0 00000+0 0 9999
2 44475 0.0639 256.7236 0000693 165.0884 298.1919 1.00272152 14122
| Epoch (UTC): | 09 June 2023 04:46:04 |
| Eccentricity: | 0.0000693 |
| inclination: | 0.0639° |
| perigee height: | 35783 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 256.7236° |
| argument of perigee: | 165.0884° |
| revolutions per day: | 1.00272152 |
| mean anomaly at epoch: | 298.1919° |
| orbit number at epoch: | 1412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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