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 26064.24044832 +.00000000 +00000-0 +81932-4 0 00003
2 14148 82.5211 165.5135 0019201 271.8946 88.0071 14.85663023 07
| Epoch (UTC): | 05 March 2026 05:46:14 |
| Eccentricity: | 0.0019201 |
| inclination: | 82.5211° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 165.5135° |
| argument of perigee: | 271.8946° |
| revolutions per day: | 14.85663023 |
| mean anomaly at epoch: | 88.0071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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