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 28381U 26088.18573632 +.00000000 +00000-0 +18351-3 0 00005
2 28381 82.9535 110.8349 0032455 29.1504 41.1735 13.78617796 08
| Epoch (UTC): | 29 March 2026 04:27:27 |
| Eccentricity: | 0.0032455 |
| inclination: | 82.9535° |
| perigee height: | 945 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 110.8349° |
| argument of perigee: | 29.1504° |
| revolutions per day: | 13.78617796 |
| mean anomaly at epoch: | 41.1735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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