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 00016U 58002A 23080.44109572 .00000065 00000-0 86452-4 0 9997
2 00016 34.2605 126.6939 2025600 163.9965 203.5566 10.48818242564560
| Epoch (UTC): | 21 March 2023 10:35:10 |
| Eccentricity: | 0.2025600 |
| inclination: | 34.2605° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 126.6939° |
| argument of perigee: | 163.9965° |
| revolutions per day: | 10.48818242 |
| mean anomaly at epoch: | 203.5566° |
| orbit number at epoch: | 56456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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