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 39483U 13076A 25193.90264420 .00000009 00000-0 -82951-5 0 9991
2 39483 82.4835 20.1286 0019949 114.1604 246.1564 12.42864205523740
| Epoch (UTC): | 12 July 2025 21:39:48 |
| Eccentricity: | 0.0019949 |
| inclination: | 82.4835° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 20.1286° |
| argument of perigee: | 114.1604° |
| revolutions per day: | 12.42864205 |
| mean anomaly at epoch: | 246.1564° |
| orbit number at epoch: | 52374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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