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 00020U 26134.90955687 +.00000000 +00000-0 +86202-4 0 00002
2 00020 33.3549 26.7406 1638117 235.2064 108.3444 11.61947901 08
| Epoch (UTC): | 14 May 2026 21:49:45 |
| Eccentricity: | 0.1638117 |
| inclination: | 33.3549° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 26.7406° |
| argument of perigee: | 235.2064° |
| revolutions per day: | 11.61947901 |
| mean anomaly at epoch: | 108.3444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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