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 26041.49232300 +.00000000 +00000-0 +32547-3 0 00008
2 14208 97.6135 45.0593 0020858 332.2931 27.7200 15.37714292 09
| Epoch (UTC): | 10 February 2026 11:48:56 |
| Eccentricity: | 0.0020858 |
| inclination: | 97.6135° |
| perigee height: | 439 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 45.0593° |
| argument of perigee: | 332.2931° |
| revolutions per day: | 15.37714292 |
| mean anomaly at epoch: | 27.7200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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