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 26017.93037818 +.00000000 +00000-0 +29547-3 0 00003
2 14208 97.6110 20.6537 0024094 54.4167 305.9317 15.36978671 01
| Epoch (UTC): | 17 January 2026 22:19:44 |
| Eccentricity: | 0.0024094 |
| inclination: | 97.6110° |
| perigee height: | 439 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 20.6537° |
| argument of perigee: | 54.4167° |
| revolutions per day: | 15.36978671 |
| mean anomaly at epoch: | 305.9317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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