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 38354U 26150.64426126 +.00000000 +00000-0 -10342-2 0 00004
2 38354 100.7368 355.0948 0025137 332.5700 27.4085 13.18381866 03
| Epoch (UTC): | 30 May 2026 15:27:44 |
| Eccentricity: | 0.0025137 |
| inclination: | 100.7368° |
| perigee height: | 1172 km |
| apogee height: | 1210 km |
| right ascension of ascending node: | 355.0948° |
| argument of perigee: | 332.5700° |
| revolutions per day: | 13.18381866 |
| mean anomaly at epoch: | 27.4085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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