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 26099.77389296 +.00000000 +00000-0 +95266-3 0 00005
2 43881 97.6112 35.0026 0004048 154.9436 205.2018 15.60310478 09
| Epoch (UTC): | 09 April 2026 18:34:24 |
| Eccentricity: | 0.0004048 |
| inclination: | 97.6112° |
| perigee height: | 384 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 35.0026° |
| argument of perigee: | 154.9436° |
| revolutions per day: | 15.60310478 |
| mean anomaly at epoch: | 205.2018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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