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 26073.56519786 +.00000000 +00000-0 +38864-3 0 00005
2 14208 97.6141 78.3274 0020581 207.3916 152.6245 15.38546539 04
| Epoch (UTC): | 14 March 2026 13:33:53 |
| Eccentricity: | 0.0020581 |
| inclination: | 97.6141° |
| perigee height: | 436 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 78.3274° |
| argument of perigee: | 207.3916° |
| revolutions per day: | 15.38546539 |
| mean anomaly at epoch: | 152.6245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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