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 55347U 26145.55975286 +.00000000 +00000-0 +24605-4 0 00003
2 55347 43.0037 228.9510 0001704 270.9743 89.0913 15.27577764 05
| Epoch (UTC): | 25 May 2026 13:26:02 |
| Eccentricity: | 0.0001704 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 228.9510° |
| argument of perigee: | 270.9743° |
| revolutions per day: | 15.27577764 |
| mean anomaly at epoch: | 89.0913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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