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 26065.76004360 +.00000000 +00000-0 +38045-3 0 00006
2 14208 97.6141 70.2262 0019888 237.2042 122.7287 15.38329896 01
| Epoch (UTC): | 06 March 2026 18:14:27 |
| Eccentricity: | 0.0019888 |
| inclination: | 97.6141° |
| perigee height: | 437 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 70.2262° |
| argument of perigee: | 237.2042° |
| revolutions per day: | 15.38329896 |
| mean anomaly at epoch: | 122.7287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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