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 00011U 59001A 23275.81240994 .00000613 00000-0 30603-3 0 9998
2 00011 32.8705 217.6190 1461433 204.5599 147.7934 11.87322991417786
| Epoch (UTC): | 02 October 2023 19:29:52 |
| Eccentricity: | 0.1461433 |
| inclination: | 32.8705° |
| perigee height: | 552 km |
| apogee height: | 2924 km |
| right ascension of ascending node: | 217.6190° |
| argument of perigee: | 204.5599° |
| revolutions per day: | 11.87322991 |
| mean anomaly at epoch: | 147.7934° |
| orbit number at epoch: | 41778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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