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 26075.84150926 +.00000000 +00000-0 +24959-3 0 00005
2 14208 97.6136 80.6902 0020843 198.9821 161.0649 15.38595284 06
| Epoch (UTC): | 16 March 2026 20:11:46 |
| Eccentricity: | 0.0020843 |
| inclination: | 97.6136° |
| perigee height: | 436 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 80.6902° |
| argument of perigee: | 198.9821° |
| revolutions per day: | 15.38595284 |
| mean anomaly at epoch: | 161.0649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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