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 55349U 26145.57519170 +.00000000 +00000-0 +17932-2 0 00006
2 55349 43.0020 229.0607 0001357 281.1326 78.9373 15.27317738 03
| Epoch (UTC): | 25 May 2026 13:48:16 |
| Eccentricity: | 0.0001357 |
| inclination: | 43.0020° |
| perigee height: | 483 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 229.0607° |
| argument of perigee: | 281.1326° |
| revolutions per day: | 15.27317738 |
| mean anomaly at epoch: | 78.9373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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