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 56690U 26145.22015477 +.00000000 +00000-0 +71318-4 0 00009
2 56690 43.0044 209.1239 0002186 270.5783 89.4818 15.27583882 05
| Epoch (UTC): | 25 May 2026 05:17:01 |
| Eccentricity: | 0.0002186 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 209.1239° |
| argument of perigee: | 270.5783° |
| revolutions per day: | 15.27583882 |
| mean anomaly at epoch: | 89.4818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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