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 26110.47636353 +.00000000 +00000-0 +41972-4 0 00007
2 03890 99.7140 353.4264 0040205 102.7741 70.6999 13.42668723 04
| Epoch (UTC): | 20 April 2026 11:25:57 |
| Eccentricity: | 0.0040205 |
| inclination: | 99.7140° |
| perigee height: | 1069 km |
| apogee height: | 1129 km |
| right ascension of ascending node: | 353.4264° |
| argument of perigee: | 102.7741° |
| revolutions per day: | 13.42668723 |
| mean anomaly at epoch: | 70.6999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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