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 25136.93393319 .00000278 00000-0 10233-3 0 9996
2 16682 74.0246 315.2349 0015001 310.3386 158.0233 14.37113266 45821
| Epoch (UTC): | 16 May 2025 22:24:51 |
| Eccentricity: | 0.0015001 |
| inclination: | 74.0246° |
| perigee height: | 757 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 315.2349° |
| argument of perigee: | 310.3386° |
| revolutions per day: | 14.37113266 |
| mean anomaly at epoch: | 158.0233° |
| orbit number at epoch: | 4582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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