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 23155.49292274 .00000444 00000-0 93949-4 0 9990
2 37839 19.9594 199.9531 0019075 78.9714 60.1035 14.12958518601987
| Epoch (UTC): | 04 June 2023 11:49:48 |
| Eccentricity: | 0.0019075 |
| inclination: | 19.9594° |
| perigee height: | 835 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 199.9531° |
| argument of perigee: | 78.9714° |
| revolutions per day: | 14.12958518 |
| mean anomaly at epoch: | 60.1035° |
| orbit number at epoch: | 60198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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