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 23160.51582632 .00000130 00000-0 53558-4 0 9998
2 16682 74.0237 176.1023 0015121 339.4768 134.4481 14.36277809944254
| Epoch (UTC): | 09 June 2023 12:22:47 |
| Eccentricity: | 0.0015121 |
| inclination: | 74.0237° |
| perigee height: | 760 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 176.1023° |
| argument of perigee: | 339.4768° |
| revolutions per day: | 14.36277809 |
| mean anomaly at epoch: | 134.4481° |
| orbit number at epoch: | 94425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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