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 44387U 19038A 23343.08318272 .00000041 00000-0 37562-4 0 9995
2 44387 98.8014 306.8416 0001938 122.9749 237.1616 14.23832529230191
| Epoch (UTC): | 09 December 2023 01:59:46 |
| Eccentricity: | 0.0001938 |
| inclination: | 98.8014° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 306.8416° |
| argument of perigee: | 122.9749° |
| revolutions per day: | 14.23832529 |
| mean anomaly at epoch: | 237.1616° |
| orbit number at epoch: | 23019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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