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 16409U 85119B 25197.93691406 .00000038 00000-0 20621-4 0 9992
2 16409 82.5376 169.3336 0015403 20.6456 339.5323 13.84909957999077
| Epoch (UTC): | 16 July 2025 22:29:09 |
| Eccentricity: | 0.0015403 |
| inclination: | 82.5376° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 169.3336° |
| argument of perigee: | 20.6456° |
| revolutions per day: | 13.84909957 |
| mean anomaly at epoch: | 339.5323° |
| orbit number at epoch: | 99907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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