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 25338U 98030A 24357.81899077 .00000335 00000-0 15591-3 0 9996
2 25338 98.5525 20.8785 0011071 129.6655 230.5504 14.26831946384087
| Epoch (UTC): | 22 December 2024 19:39:20 |
| Eccentricity: | 0.0011071 |
| inclination: | 98.5525° |
| perigee height: | 794 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 20.8785° |
| argument of perigee: | 129.6655° |
| revolutions per day: | 14.26831946 |
| mean anomaly at epoch: | 230.5504° |
| orbit number at epoch: | 38408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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