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 14208U 26100.09559580 +.00000000 +00000-0 +27902-3 0 00001
2 14208 97.6141 105.8812 0023156 115.5732 244.7910 15.39203608 05
| Epoch (UTC): | 10 April 2026 02:17:39 |
| Eccentricity: | 0.0023156 |
| inclination: | 97.6141° |
| perigee height: | 433 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 105.8812° |
| argument of perigee: | 115.5732° |
| revolutions per day: | 15.39203608 |
| mean anomaly at epoch: | 244.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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