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 23156.90978372 .00000547 00000-0 61525-4 0 9997
2 16496 82.5234 126.5107 0020741 74.9263 342.2443 14.84703822999568
| Epoch (UTC): | 05 June 2023 21:50:05 |
| Eccentricity: | 0.0020741 |
| inclination: | 82.5234° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 126.5107° |
| argument of perigee: | 74.9263° |
| revolutions per day: | 14.84703822 |
| mean anomaly at epoch: | 342.2443° |
| orbit number at epoch: | 99956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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