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 30492U 99025AHE 24357.52283663 .00024585 00000-0 75815-2 0 9991
2 30492 102.3323 210.2028 0126176 275.5182 83.1610 14.36882422917637
| Epoch (UTC): | 22 December 2024 12:32:53 |
| Eccentricity: | 0.0126176 |
| inclination: | 102.3323° |
| perigee height: | 678 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 210.2028° |
| argument of perigee: | 275.5182° |
| revolutions per day: | 14.36882422 |
| mean anomaly at epoch: | 83.1610° |
| orbit number at epoch: | 91763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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