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 33493U 09002B 24258.71096908 .00085862 00000-0 32470-2 0 9991
2 33493 98.1947 314.4225 0009622 293.9573 66.0655 15.26569066852672
| Epoch (UTC): | 14 September 2024 17:03:47 |
| Eccentricity: | 0.0009622 |
| inclination: | 98.1947° |
| perigee height: | 479 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 314.4225° |
| argument of perigee: | 293.9573° |
| revolutions per day: | 15.26569066 |
| mean anomaly at epoch: | 66.0655° |
| orbit number at epoch: | 85267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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