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 55331U 26145.52648977 +.00000000 +00000-0 +26803-4 0 00009
2 55331 43.0016 229.5604 0001334 270.0157 90.0542 15.27576979 02
| Epoch (UTC): | 25 May 2026 12:38:08 |
| Eccentricity: | 0.0001334 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.5604° |
| argument of perigee: | 270.0157° |
| revolutions per day: | 15.27576979 |
| mean anomaly at epoch: | 90.0542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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