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 16369U 85116B 23151.81989764 .00000193 00000-0 17903-3 0 9996
2 16369 82.9362 170.9192 0036034 190.7553 342.1306 13.76956156880927
| Epoch (UTC): | 31 May 2023 19:40:39 |
| Eccentricity: | 0.0036034 |
| inclination: | 82.9362° |
| perigee height: | 948 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 170.9192° |
| argument of perigee: | 190.7553° |
| revolutions per day: | 13.76956156 |
| mean anomaly at epoch: | 342.1306° |
| orbit number at epoch: | 88092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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