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 14148U 83061B 22144.17978310 .00000434 00000-0 49650-4 0 9994
2 14148 82.5208 21.6104 0022227 149.2458 211.0064 14.83505118101964
| Epoch (UTC): | 24 May 2022 04:18:53 |
| Eccentricity: | 0.0022227 |
| inclination: | 82.5208° |
| perigee height: | 603 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 21.6104° |
| argument of perigee: | 149.2458° |
| revolutions per day: | 14.83505118 |
| mean anomaly at epoch: | 211.0064° |
| orbit number at epoch: | 10196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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