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 24340.56806863 .00000466 00000-0 20992-3 0 9997
2 25338 98.5539 4.0179 0010277 177.7855 182.3372 14.26817223381622
| Epoch (UTC): | 05 December 2024 13:38:01 |
| Eccentricity: | 0.0010277 |
| inclination: | 98.5539° |
| perigee height: | 795 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 4.0179° |
| argument of perigee: | 177.7855° |
| revolutions per day: | 14.26817223 |
| mean anomaly at epoch: | 182.3372° |
| orbit number at epoch: | 38162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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