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 33679U 99025DFQ 24280.89266639 .00038861 00000-0 36269-2 0 9992
2 33679 99.3852 260.7148 0224606 226.1820 132.0623 14.76869445878201
| Epoch (UTC): | 06 October 2024 21:25:26 |
| Eccentricity: | 0.0224606 |
| inclination: | 99.3852° |
| perigee height: | 481 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 260.7148° |
| argument of perigee: | 226.1820° |
| revolutions per day: | 14.76869445 |
| mean anomaly at epoch: | 132.0623° |
| orbit number at epoch: | 87820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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