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 23157.34198115 .00000571 00000-0 65139-4 0 9997
2 14820 82.5417 108.3763 0020138 67.4891 292.8454 14.84210726 98120
| Epoch (UTC): | 06 June 2023 08:12:27 |
| Eccentricity: | 0.0020138 |
| inclination: | 82.5417° |
| perigee height: | 602 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 108.3763° |
| argument of perigee: | 67.4891° |
| revolutions per day: | 14.84210726 |
| mean anomaly at epoch: | 292.8454° |
| orbit number at epoch: | 9812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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