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 32404U 26142.79330588 +.00000000 +00000-0 +00000-0 0 00004
2 32404 5.9489 35.7739 0003060 119.6380 108.9740 1.00211708 00
| Epoch (UTC): | 22 May 2026 19:02:21 |
| Eccentricity: | 0.0003060 |
| inclination: | 5.9489° |
| perigee height: | 35791 km |
| apogee height: | 35816 km |
| right ascension of ascending node: | 35.7739° |
| argument of perigee: | 119.6380° |
| revolutions per day: | 1.00211708 |
| mean anomaly at epoch: | 108.9740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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