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 26064.71191000 +.00000000 +00000-0 +81958-4 0 00003
2 14148 82.5212 165.0704 0019215 270.2120 89.6894 14.85663652 05
| Epoch (UTC): | 05 March 2026 17:05:09 |
| Eccentricity: | 0.0019215 |
| inclination: | 82.5212° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 165.0704° |
| argument of perigee: | 270.2120° |
| revolutions per day: | 14.85663652 |
| mean anomaly at epoch: | 89.6894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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