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 26074.94932412 +.00000000 +00000-0 +45375-4 0 00002
2 14148 82.5203 155.4489 0019486 233.7312 126.2104 14.85675107 05
| Epoch (UTC): | 15 March 2026 22:47:01 |
| Eccentricity: | 0.0019486 |
| inclination: | 82.5203° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 155.4489° |
| argument of perigee: | 233.7312° |
| revolutions per day: | 14.85675107 |
| mean anomaly at epoch: | 126.2104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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