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 26072.00424938 +.00000000 +00000-0 +32189-3 0 00001
2 14208 97.6145 76.7071 0020446 213.2813 146.7148 15.38504931 03
| Epoch (UTC): | 13 March 2026 00:06:07 |
| Eccentricity: | 0.0020446 |
| inclination: | 97.6145° |
| perigee height: | 437 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 76.7071° |
| argument of perigee: | 213.2813° |
| revolutions per day: | 15.38504931 |
| mean anomaly at epoch: | 146.7148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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