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 23087.76346652 .00000696 00000-0 22746-3 0 9999
2 37839 19.9604 250.8679 0018945 51.9039 68.7351 14.12916434592508
| Epoch (UTC): | 28 March 2023 18:19:23 |
| Eccentricity: | 0.0018945 |
| inclination: | 19.9604° |
| perigee height: | 836 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 250.8679° |
| argument of perigee: | 51.9039° |
| revolutions per day: | 14.12916434 |
| mean anomaly at epoch: | 68.7351° |
| orbit number at epoch: | 59250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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