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 61855U 26145.41407084 +.00000000 +00000-0 -37342-3 0 00007
2 61855 42.9998 164.5185 0001392 276.9396 83.1297 15.27605543 03
| Epoch (UTC): | 25 May 2026 09:56:15 |
| Eccentricity: | 0.0001392 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5185° |
| argument of perigee: | 276.9396° |
| revolutions per day: | 15.27605543 |
| mean anomaly at epoch: | 83.1297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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