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 52159U 22033C 23035.93641477 .00000602 00000-0 97187-4 0 9990
2 52159 97.9786 119.8054 0006502 20.0719 340.0745 14.74920621 45592
| Epoch (UTC): | 04 February 2023 22:28:26 |
| Eccentricity: | 0.0006502 |
| inclination: | 97.9786° |
| perigee height: | 641 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 119.8054° |
| argument of perigee: | 20.0719° |
| revolutions per day: | 14.74920621 |
| mean anomaly at epoch: | 340.0745° |
| orbit number at epoch: | 4559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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