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 26110.96455565 +.00000000 +00000-0 +31441-4 0 00005
2 03890 99.7140 353.8963 0040216 101.6064 270.4015 13.42668744 04
| Epoch (UTC): | 20 April 2026 23:08:57 |
| Eccentricity: | 0.0040216 |
| inclination: | 99.7140° |
| perigee height: | 1069 km |
| apogee height: | 1129 km |
| right ascension of ascending node: | 353.8963° |
| argument of perigee: | 101.6064° |
| revolutions per day: | 13.42668744 |
| mean anomaly at epoch: | 270.4015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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