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 26106.98649266 +.00000000 +00000-0 +17970-3 0 00000
2 14208 97.6127 113.0416 0023253 92.9383 267.4524 15.39303078 03
| Epoch (UTC): | 16 April 2026 23:40:32 |
| Eccentricity: | 0.0023253 |
| inclination: | 97.6127° |
| perigee height: | 432 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 113.0416° |
| argument of perigee: | 92.9383° |
| revolutions per day: | 15.39303078 |
| mean anomaly at epoch: | 267.4524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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