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 38352U 26144.89023726 +.00000000 +00000-0 +00000-0 0 00008
2 38352 1.3965 84.1640 0003055 36.8187 180.2154 1.00269155 06
| Epoch (UTC): | 24 May 2026 21:21:56 |
| Eccentricity: | 0.0003055 |
| inclination: | 1.3965° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 84.1640° |
| argument of perigee: | 36.8187° |
| revolutions per day: | 1.00269155 |
| mean anomaly at epoch: | 180.2154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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