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 39173U 13026B 23331.13189536 -.00000493 00000-0 00000-0 0 9990
2 39173 30.6698 26.7443 7638131 66.5705 352.5793 1.10511035 41939
| Epoch (UTC): | 27 November 2023 03:09:55 |
| Eccentricity: | 0.7638131 |
| inclination: | 30.6698° |
| perigee height: | 2955 km |
| apogee height: | 63324 km |
| right ascension of ascending node: | 26.7443° |
| argument of perigee: | 66.5705° |
| revolutions per day: | 1.10511035 |
| mean anomaly at epoch: | 352.5793° |
| orbit number at epoch: | 4193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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