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 23160.43765465 .00000427 00000-0 85053-4 0 9995
2 37839 19.9590 169.9496 0019015 133.1436 12.5980 14.12960345602688
| Epoch (UTC): | 09 June 2023 10:30:13 |
| Eccentricity: | 0.0019015 |
| inclination: | 19.9590° |
| perigee height: | 835 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 169.9496° |
| argument of perigee: | 133.1436° |
| revolutions per day: | 14.12960345 |
| mean anomaly at epoch: | 12.5980° |
| orbit number at epoch: | 60268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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