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 54856U 26145.41967314 +.00000000 +00000-0 +18409-4 0 00000
2 54856 43.0030 48.4044 0001158 221.5413 138.5351 15.27579030 02
| Epoch (UTC): | 25 May 2026 10:04:19 |
| Eccentricity: | 0.0001158 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.4044° |
| argument of perigee: | 221.5413° |
| revolutions per day: | 15.27579030 |
| mean anomaly at epoch: | 138.5351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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