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 23152.47423128 .00000545 00000-0 61242-4 0 9993
2 16496 82.5232 130.6715 0020781 88.4220 35.7085 14.84699043 20003
| Epoch (UTC): | 01 June 2023 11:22:53 |
| Eccentricity: | 0.0020781 |
| inclination: | 82.5232° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 130.6715° |
| argument of perigee: | 88.4220° |
| revolutions per day: | 14.84699043 |
| mean anomaly at epoch: | 35.7085° |
| orbit number at epoch: | 2000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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