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 26064.97946573 +.00000000 +00000-0 +32228-3 0 00006
2 14208 97.6138 69.4161 0019835 240.3672 119.5597 15.38308154 03
| Epoch (UTC): | 05 March 2026 23:30:25 |
| Eccentricity: | 0.0019835 |
| inclination: | 97.6138° |
| perigee height: | 438 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 69.4161° |
| argument of perigee: | 240.3672° |
| revolutions per day: | 15.38308154 |
| mean anomaly at epoch: | 119.5597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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