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 54850U 26145.45550878 +.00000000 +00000-0 -24849-4 0 00007
2 54850 43.0074 47.8229 0002382 282.2672 77.7913 15.27593115 01
| Epoch (UTC): | 25 May 2026 10:55:55 |
| Eccentricity: | 0.0002382 |
| inclination: | 43.0074° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 47.8229° |
| argument of perigee: | 282.2672° |
| revolutions per day: | 15.27593115 |
| mean anomaly at epoch: | 77.7913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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