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 00005U 58002B 23275.91062299 .00000230 00000-0 30364-3 0 9991
2 00005 34.2446 123.2630 1844691 4.4816 357.0067 10.85089181335867
| Epoch (UTC): | 02 October 2023 21:51:17 |
| Eccentricity: | 0.1844691 |
| inclination: | 34.2446° |
| perigee height: | 650 km |
| apogee height: | 3830 km |
| right ascension of ascending node: | 123.2630° |
| argument of perigee: | 4.4816° |
| revolutions per day: | 10.85089181 |
| mean anomaly at epoch: | 357.0067° |
| orbit number at epoch: | 33586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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