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 is defined by the following mean orbital elements,
1 14148U 26069.22446300 +.00000000 +00000-0 +68503-4 0 00001
2 14148 82.5212 160.8297 0019267 254.0839 105.8254 14.85669365 07
| Epoch (UTC): | 10 March 2026 05:23:13 |
| Eccentricity: | 0.0019267 |
| inclination: | 82.5212° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 160.8297° |
| argument of perigee: | 254.0839° |
| revolutions per day: | 14.85669365 |
| mean anomaly at epoch: | 105.8254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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