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 38326U 10051H 24285.46322960 .00193413 00000-0 26611-1 0 9990
2 38326 97.7759 356.0394 0141822 79.0246 282.6879 14.70536313731268
| Epoch (UTC): | 11 October 2024 11:07:03 |
| Eccentricity: | 0.0141822 |
| inclination: | 97.7759° |
| perigee height: | 559 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 356.0394° |
| argument of perigee: | 79.0246° |
| revolutions per day: | 14.70536313 |
| mean anomaly at epoch: | 282.6879° |
| orbit number at epoch: | 73126 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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