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 16496U 86006B 23147.07184612 .00000486 00000-0 54387-4 0 9991
2 16496 82.5228 135.7395 0020729 104.8985 321.8390 14.84693292 19209
| Epoch (UTC): | 27 May 2023 01:43:27 |
| Eccentricity: | 0.0020729 |
| inclination: | 82.5228° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 135.7395° |
| argument of perigee: | 104.8985° |
| revolutions per day: | 14.84693292 |
| mean anomaly at epoch: | 321.8390° |
| orbit number at epoch: | 1920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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