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 26053.66240288 +.00000000 +00000-0 +28533-4 0 00000
2 03890 99.7238 298.7135 0038736 241.8631 134.6290 13.42665664 05
| Epoch (UTC): | 22 February 2026 15:53:51 |
| Eccentricity: | 0.0038736 |
| inclination: | 99.7238° |
| perigee height: | 1070 km |
| apogee height: | 1128 km |
| right ascension of ascending node: | 298.7135° |
| argument of perigee: | 241.8631° |
| revolutions per day: | 13.42665664 |
| mean anomaly at epoch: | 134.6290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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