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 26074.61256808 +.00000000 +00000-0 +45180-4 0 00008
2 14148 82.5204 155.7654 0019473 234.9071 125.0320 14.85674760 05
| Epoch (UTC): | 15 March 2026 14:42:05 |
| Eccentricity: | 0.0019473 |
| inclination: | 82.5204° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 155.7654° |
| argument of perigee: | 234.9071° |
| revolutions per day: | 14.85674760 |
| mean anomaly at epoch: | 125.0320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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