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 40128U 26143.08459647 +.00000000 +00000-0 +00000-0 0 00007
2 40128 48.9035 274.4648 1670806 178.4149 182.2129 1.85519899 03
| Epoch (UTC): | 23 May 2026 02:01:49 |
| Eccentricity: | 0.1670806 |
| inclination: | 48.9035° |
| perigee height: | 16925 km |
| apogee height: | 26274 km |
| right ascension of ascending node: | 274.4648° |
| argument of perigee: | 178.4149° |
| revolutions per day: | 1.85519899 |
| mean anomaly at epoch: | 182.2129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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