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 26032.15797675 +.00000000 +00000-0 +57193-4 0 00002
2 03890 99.7269 277.9886 0038797 295.4766 229.9837 13.42664468 08
| Epoch (UTC): | 01 February 2026 03:47:29 |
| Eccentricity: | 0.0038797 |
| inclination: | 99.7269° |
| perigee height: | 1070 km |
| apogee height: | 1128 km |
| right ascension of ascending node: | 277.9886° |
| argument of perigee: | 295.4766° |
| revolutions per day: | 13.42664468 |
| mean anomaly at epoch: | 229.9837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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