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 25188.90597923 .00000035 00000-0 17736-4 0 9998
2 16409 82.5366 176.5233 0015891 44.8733 315.3710 13.84909698997824
| Epoch (UTC): | 07 July 2025 21:44:36 |
| Eccentricity: | 0.0015891 |
| inclination: | 82.5366° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 176.5233° |
| argument of perigee: | 44.8733° |
| revolutions per day: | 13.84909698 |
| mean anomaly at epoch: | 315.3710° |
| orbit number at epoch: | 99782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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