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 26066.15032831 +.00000000 +00000-0 +35361-3 0 00002
2 14208 97.6142 70.6312 0019916 235.6705 124.2655 15.38339493 02
| Epoch (UTC): | 07 March 2026 03:36:28 |
| Eccentricity: | 0.0019916 |
| inclination: | 97.6142° |
| perigee height: | 437 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 70.6312° |
| argument of perigee: | 235.6705° |
| revolutions per day: | 15.38339493 |
| mean anomaly at epoch: | 124.2655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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