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 38044U 26145.42185225 +.00000000 +00000-0 +75710-4 0 00003
2 38044 52.0144 37.7441 0000658 58.4223 113.7062 12.62268594 01
| Epoch (UTC): | 25 May 2026 10:07:28 |
| Eccentricity: | 0.0000658 |
| inclination: | 52.0144° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 37.7441° |
| argument of perigee: | 58.4223° |
| revolutions per day: | 12.62268594 |
| mean anomaly at epoch: | 113.7062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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