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 26067.74273091 +.00000000 +00000-0 +82107-4 0 00007
2 14148 82.5212 162.2222 0019232 259.3968 100.5082 14.85667869 02
| Epoch (UTC): | 08 March 2026 17:49:31 |
| Eccentricity: | 0.0019232 |
| inclination: | 82.5212° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 162.2222° |
| argument of perigee: | 259.3968° |
| revolutions per day: | 14.85667869 |
| mean anomaly at epoch: | 100.5082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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