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 38861U 26145.36553928 +.00000000 +00000-0 +18861-3 0 00005
2 38861 97.5971 130.3098 0013740 293.9173 66.0606 14.91226541 08
| Epoch (UTC): | 25 May 2026 08:46:22 |
| Eccentricity: | 0.0013740 |
| inclination: | 97.5971° |
| perigee height: | 585 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 130.3098° |
| argument of perigee: | 293.9173° |
| revolutions per day: | 14.91226541 |
| mean anomaly at epoch: | 66.0606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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