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 55345U 26145.48345867 +.00000000 +00000-0 -12260-4 0 00004
2 55345 43.0020 215.3570 0001178 276.6332 83.4385 15.27570445 03
| Epoch (UTC): | 25 May 2026 11:36:10 |
| Eccentricity: | 0.0001178 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.3570° |
| argument of perigee: | 276.6332° |
| revolutions per day: | 15.27570445 |
| mean anomaly at epoch: | 83.4385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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