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 26162.23433683 +.00000000 +00000-0 +35874-4 0 00001
2 14148 82.5185 73.3667 0019475 310.7168 49.2356 14.85744651 07
| Epoch (UTC): | 11 June 2026 05:37:26 |
| Eccentricity: | 0.0019475 |
| inclination: | 82.5185° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 73.3667° |
| argument of perigee: | 310.7168° |
| revolutions per day: | 14.85744651 |
| mean anomaly at epoch: | 49.2356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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