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 55781U 26145.11784125 +.00000000 +00000-0 +47415-5 0 00002
2 55781 70.0004 31.6967 0002500 270.7228 89.3645 14.98333792 00
| Epoch (UTC): | 25 May 2026 02:49:41 |
| Eccentricity: | 0.0002500 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.6967° |
| argument of perigee: | 270.7228° |
| revolutions per day: | 14.98333792 |
| mean anomaly at epoch: | 89.3645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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