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 23038.39852307 .00003063 00000-0 16241-2 0 9998
2 00011 32.8788 31.1176 1463512 301.0601 45.4344 11.86470751389567
| Epoch (UTC): | 07 February 2023 09:33:52 |
| Eccentricity: | 0.1463512 |
| inclination: | 32.8788° |
| perigee height: | 553 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 31.1176° |
| argument of perigee: | 301.0601° |
| revolutions per day: | 11.86470751 |
| mean anomaly at epoch: | 45.4344° |
| orbit number at epoch: | 38956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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