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 37839U 11058B 23080.89480644 .00000597 00000-0 17511-3 0 9990
2 37839 19.9614 292.5391 0018800 336.2650 51.2850 14.12910272591426
| Epoch (UTC): | 21 March 2023 21:28:31 |
| Eccentricity: | 0.0018800 |
| inclination: | 19.9614° |
| perigee height: | 836 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 292.5391° |
| argument of perigee: | 336.2650° |
| revolutions per day: | 14.12910272 |
| mean anomaly at epoch: | 51.2850° |
| orbit number at epoch: | 59142 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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