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 03891U 26088.10181602 +.00000000 +00000-0 +36284-4 0 00004
2 03891 99.6617 323.0195 0040301 88.0341 68.1119 13.42973499 03
| Epoch (UTC): | 29 March 2026 02:26:36 |
| Eccentricity: | 0.0040301 |
| inclination: | 99.6617° |
| perigee height: | 1068 km |
| apogee height: | 1128 km |
| right ascension of ascending node: | 323.0195° |
| argument of perigee: | 88.0341° |
| revolutions per day: | 13.42973499 |
| mean anomaly at epoch: | 68.1119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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