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 26075.95959215 +.00000000 +00000-0 +45452-4 0 00000
2 14148 82.5201 154.4994 0019539 230.1896 129.7601 14.85676045 02
| Epoch (UTC): | 16 March 2026 23:01:48 |
| Eccentricity: | 0.0019539 |
| inclination: | 82.5201° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 154.4994° |
| argument of perigee: | 230.1896° |
| revolutions per day: | 14.85676045 |
| mean anomaly at epoch: | 129.7601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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