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 01002U 26128.71570286 +.00000000 +00000-0 -18601-2 0 00000
2 01002 32.1380 138.2126 0015350 128.5180 231.6695 9.88355254 05
| Epoch (UTC): | 08 May 2026 17:10:36 |
| Eccentricity: | 0.0015350 |
| inclination: | 32.1380° |
| perigee height: | 2780 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 138.2126° |
| argument of perigee: | 128.5180° |
| revolutions per day: | 9.88355254 |
| mean anomaly at epoch: | 231.6695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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