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 39765U 14028E 23273.11733566 .00000022 00000-0 38245-4 0 9994
2 39765 82.4530 201.1450 0231543 168.1325 192.5368 12.82863441438166
| Epoch (UTC): | 30 September 2023 02:48:57 |
| Eccentricity: | 0.0231543 |
| inclination: | 82.4530° |
| perigee height: | 1151 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 201.1450° |
| argument of perigee: | 168.1325° |
| revolutions per day: | 12.82863441 |
| mean anomaly at epoch: | 192.5368° |
| orbit number at epoch: | 43816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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