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 25343.11324693 .00000237 00000-0 11495-3 0 9992
2 25338 98.5222 3.7446 0010272 178.4397 181.6818 14.27068555434182
| Epoch (UTC): | 09 December 2025 02:43:04 |
| Eccentricity: | 0.0010272 |
| inclination: | 98.5222° |
| perigee height: | 794 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 3.7446° |
| argument of perigee: | 178.4397° |
| revolutions per day: | 14.27068555 |
| mean anomaly at epoch: | 181.6818° |
| orbit number at epoch: | 43418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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