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 23344.35901297 .00000541 00000-0 26602-3 0 9998
2 00011 32.8780 319.5178 1460332 232.5989 113.2670 11.87427793425935
| Epoch (UTC): | 10 December 2023 08:36:58 |
| Eccentricity: | 0.1460332 |
| inclination: | 32.8780° |
| perigee height: | 552 km |
| apogee height: | 2923 km |
| right ascension of ascending node: | 319.5178° |
| argument of perigee: | 232.5989° |
| revolutions per day: | 11.87427793 |
| mean anomaly at epoch: | 113.2670° |
| orbit number at epoch: | 42593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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