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 38011U 26145.62313358 +.00000000 +00000-0 +19675-3 0 00006
2 38011 97.8076 206.5603 0001464 95.4552 59.8874 14.82450500 09
| Epoch (UTC): | 25 May 2026 14:57:18 |
| Eccentricity: | 0.0001464 |
| inclination: | 97.8076° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 206.5603° |
| argument of perigee: | 95.4552° |
| revolutions per day: | 14.82450500 |
| mean anomaly at epoch: | 59.8874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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