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 38356U 26145.62633274 +.00000000 +00000-0 +00000-0 0 00009
2 38356 0.0187 307.8296 0003068 119.7290 207.1366 1.00272367 07
| Epoch (UTC): | 25 May 2026 15:01:55 |
| Eccentricity: | 0.0003068 |
| inclination: | 0.0187° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 307.8296° |
| argument of perigee: | 119.7290° |
| revolutions per day: | 1.00272367 |
| mean anomaly at epoch: | 207.1366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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