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 38340U 12025D 24278.82764745 .00017488 00000-0 21226-2 0 9997
2 38340 98.1685 20.9087 0009921 48.4298 311.7764 14.83576977656473
| Epoch (UTC): | 04 October 2024 19:51:48 |
| Eccentricity: | 0.0009921 |
| inclination: | 98.1685° |
| perigee height: | 611 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 20.9087° |
| argument of perigee: | 48.4298° |
| revolutions per day: | 14.83576977 |
| mean anomaly at epoch: | 311.7764° |
| orbit number at epoch: | 65647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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