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 38093U 26098.93401110 +.00000000 +00000-0 +00000-0 0 00000
2 38093 5.3355 47.1838 0059109 0.1256 26.1651 1.00271334 07
| Epoch (UTC): | 08 April 2026 22:24:58 |
| Eccentricity: | 0.0059109 |
| inclination: | 5.3355° |
| perigee height: | 35537 km |
| apogee height: | 36036 km |
| right ascension of ascending node: | 47.1838° |
| argument of perigee: | 0.1256° |
| revolutions per day: | 1.00271334 |
| mean anomaly at epoch: | 26.1651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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