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 55034U 26101.46346073 +.00000000 +00000-0 +19803-3 0 00007
2 55034 97.3264 161.0473 0008219 11.0376 349.1044 15.32448979 07
| Epoch (UTC): | 11 April 2026 11:07:23 |
| Eccentricity: | 0.0008219 |
| inclination: | 97.3264° |
| perigee height: | 463 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 161.0473° |
| argument of perigee: | 11.0376° |
| revolutions per day: | 15.32448979 |
| mean anomaly at epoch: | 349.1044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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