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 56536U 26145.51543963 +.00000000 +00000-0 +30279-4 0 00007
2 56536 43.0019 152.9538 0001115 273.3009 86.7715 15.27578221 03
| Epoch (UTC): | 25 May 2026 12:22:13 |
| Eccentricity: | 0.0001115 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 152.9538° |
| argument of perigee: | 273.3009° |
| revolutions per day: | 15.27578221 |
| mean anomaly at epoch: | 86.7715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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