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 14820U 84027B 23150.39795915 .00000496 00000-0 56224-4 0 9997
2 14820 82.5409 114.8698 0020261 88.5729 271.7808 14.84203027 97091
| Epoch (UTC): | 30 May 2023 09:33:03 |
| Eccentricity: | 0.0020261 |
| inclination: | 82.5409° |
| perigee height: | 602 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 114.8698° |
| argument of perigee: | 88.5729° |
| revolutions per day: | 14.84203027 |
| mean anomaly at epoch: | 271.7808° |
| orbit number at epoch: | 9709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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