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 43188U 18014J 25341.13703893 .00010344 00000-0 56854-3 0 9990
2 43188 97.5505 242.4256 0008334 330.4854 29.5906 15.14253518429671
| Epoch (UTC): | 07 December 2025 03:17:20 |
| Eccentricity: | 0.0008334 |
| inclination: | 97.5505° |
| perigee height: | 517 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 242.4256° |
| argument of perigee: | 330.4854° |
| revolutions per day: | 15.14253518 |
| mean anomaly at epoch: | 29.5906° |
| orbit number at epoch: | 42967 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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