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 23156.87005864 .00000557 00000-0 63486-4 0 9999
2 14820 82.5416 108.8176 0020153 68.9215 291.4153 14.84210146 98054
| Epoch (UTC): | 05 June 2023 20:52:53 |
| Eccentricity: | 0.0020153 |
| inclination: | 82.5416° |
| perigee height: | 602 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 108.8176° |
| argument of perigee: | 68.9215° |
| revolutions per day: | 14.84210146 |
| mean anomaly at epoch: | 291.4153° |
| orbit number at epoch: | 9805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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