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 26071.71646374 +.00000000 +00000-0 +64818-4 0 00006
2 14148 82.5209 158.4875 0019337 245.1703 114.7503 14.85672381 05
| Epoch (UTC): | 12 March 2026 17:11:42 |
| Eccentricity: | 0.0019337 |
| inclination: | 82.5209° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 158.4875° |
| argument of perigee: | 245.1703° |
| revolutions per day: | 14.85672381 |
| mean anomaly at epoch: | 114.7503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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