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 39428U 26131.22870637 +.00000000 +00000-0 +40087-3 0 00009
2 39428 97.8338 51.5849 0074364 331.0081 28.7018 14.94657640 00
| Epoch (UTC): | 11 May 2026 05:29:20 |
| Eccentricity: | 0.0074364 |
| inclination: | 97.8338° |
| perigee height: | 532 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 51.5849° |
| argument of perigee: | 331.0081° |
| revolutions per day: | 14.94657640 |
| mean anomaly at epoch: | 28.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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