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 39206U 26088.14926691 +.00000000 +00000-0 +00000-0 0 00005
2 39206 4.8360 45.3739 0051400 182.8698 183.9932 1.00272153 02
| Epoch (UTC): | 29 March 2026 03:34:56 |
| Eccentricity: | 0.0051400 |
| inclination: | 4.8360° |
| perigee height: | 35570 km |
| apogee height: | 36003 km |
| right ascension of ascending node: | 45.3739° |
| argument of perigee: | 182.8698° |
| revolutions per day: | 1.00272153 |
| mean anomaly at epoch: | 183.9932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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