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 03890U 26133.42734838 +.00000000 +00000-0 +22615-4 0 00007
2 03890 99.7107 15.5119 0040099 47.6299 125.7440 13.42669938 00
| Epoch (UTC): | 13 May 2026 10:15:22 |
| Eccentricity: | 0.0040099 |
| inclination: | 99.7107° |
| perigee height: | 1069 km |
| apogee height: | 1129 km |
| right ascension of ascending node: | 15.5119° |
| argument of perigee: | 47.6299° |
| revolutions per day: | 13.42669938 |
| mean anomaly at epoch: | 125.7440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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