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 26073.24000353 +.00000000 +00000-0 +35306-3 0 00003
2 14208 97.6142 77.9899 0020559 208.6402 151.3715 15.38536352 02
| Epoch (UTC): | 14 March 2026 05:45:36 |
| Eccentricity: | 0.0020559 |
| inclination: | 97.6142° |
| perigee height: | 436 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 77.9899° |
| argument of perigee: | 208.6402° |
| revolutions per day: | 15.38536352 |
| mean anomaly at epoch: | 151.3715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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