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 13028U 82001B 23270.85023051 .00000478 00000-0 16350-3 0 9990
2 13028 74.0397 122.5849 0019629 354.3160 5.7768 14.38836159186934
| Epoch (UTC): | 27 September 2023 20:24:19 |
| Eccentricity: | 0.0019629 |
| inclination: | 74.0397° |
| perigee height: | 748 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 122.5849° |
| argument of perigee: | 354.3160° |
| revolutions per day: | 14.38836159 |
| mean anomaly at epoch: | 5.7768° |
| orbit number at epoch: | 18693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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