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 43881U 26077.55335786 +.00000000 +00000-0 +84399-3 0 00007
2 43881 97.6119 11.2571 0002040 29.8431 330.2939 15.56192163 07
| Epoch (UTC): | 18 March 2026 13:16:50 |
| Eccentricity: | 0.0002040 |
| inclination: | 97.6119° |
| perigee height: | 397 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 11.2571° |
| argument of perigee: | 29.8431° |
| revolutions per day: | 15.56192163 |
| mean anomaly at epoch: | 330.2939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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