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 54844U 26145.49725241 +.00000000 +00000-0 +28713-4 0 00005
2 54844 43.0075 61.9619 0001788 275.8964 84.1684 15.27581750 05
| Epoch (UTC): | 25 May 2026 11:56:02 |
| Eccentricity: | 0.0001788 |
| inclination: | 43.0075° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 61.9619° |
| argument of perigee: | 275.8964° |
| revolutions per day: | 15.27581750 |
| mean anomaly at epoch: | 84.1684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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