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 55340U 26145.50208162 +.00000000 +00000-0 +80563-4 0 00008
2 55340 43.0026 229.3806 0001828 273.0860 86.9783 15.27583942 06
| Epoch (UTC): | 25 May 2026 12:02:59 |
| Eccentricity: | 0.0001828 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.3806° |
| argument of perigee: | 273.0860° |
| revolutions per day: | 15.27583942 |
| mean anomaly at epoch: | 86.9783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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