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 16792U 86046B 23151.92978580 .00000474 00000-0 54095-4 0 9991
2 16792 82.4810 315.5605 0023214 334.2049 25.8007 14.83798862976125
| Epoch (UTC): | 31 May 2023 22:18:53 |
| Eccentricity: | 0.0023214 |
| inclination: | 82.4810° |
| perigee height: | 601 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 315.5605° |
| argument of perigee: | 334.2049° |
| revolutions per day: | 14.83798862 |
| mean anomaly at epoch: | 25.8007° |
| orbit number at epoch: | 97612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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