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 56542U 26145.51929072 +.00000000 +00000-0 -10232-4 0 00001
2 56542 43.0013 152.9786 0001341 272.6759 87.3939 15.27571857 07
| Epoch (UTC): | 25 May 2026 12:27:46 |
| Eccentricity: | 0.0001341 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 152.9786° |
| argument of perigee: | 272.6759° |
| revolutions per day: | 15.27571857 |
| mean anomaly at epoch: | 87.3939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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