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 25131.92872078 .00000291 00000-0 10683-3 0 9998
2 16682 74.0249 324.4470 0014852 320.2050 183.5930 14.37109984 45102
| Epoch (UTC): | 11 May 2025 22:17:21 |
| Eccentricity: | 0.0014852 |
| inclination: | 74.0249° |
| perigee height: | 757 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 324.4470° |
| argument of perigee: | 320.2050° |
| revolutions per day: | 14.37109984 |
| mean anomaly at epoch: | 183.5930° |
| orbit number at epoch: | 4510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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