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 16682U 86030B 25339.07253707 .00000619 00000-0 21643-3 0 9998
2 16682 74.0250 303.2005 0015673 253.1880 179.1189 14.37245130 74866
| Epoch (UTC): | 05 December 2025 01:44:27 |
| Eccentricity: | 0.0015673 |
| inclination: | 74.0250° |
| perigee height: | 756 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 303.2005° |
| argument of perigee: | 253.1880° |
| revolutions per day: | 14.37245130 |
| mean anomaly at epoch: | 179.1189° |
| orbit number at epoch: | 7486 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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