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 24357.88623326 .00001217 00000-0 62177-3 0 9993
2 00011 32.8761 332.0339 1453243 219.0378 129.5986 11.88986910470974
| Epoch (UTC): | 22 December 2024 21:16:10 |
| Eccentricity: | 0.1453243 |
| inclination: | 32.8761° |
| perigee height: | 552 km |
| apogee height: | 2909 km |
| right ascension of ascending node: | 332.0339° |
| argument of perigee: | 219.0378° |
| revolutions per day: | 11.88986910 |
| mean anomaly at epoch: | 129.5986° |
| orbit number at epoch: | 47097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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