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 54743U 26145.58372844 +.00000000 +00000-0 +00000-0 0 00005
2 54743 0.7588 27.0437 0000803 3.8903 62.0893 1.00274816 07
| Epoch (UTC): | 25 May 2026 14:00:34 |
| Eccentricity: | 0.0000803 |
| inclination: | 0.7588° |
| perigee height: | 35782 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 27.0437° |
| argument of perigee: | 3.8903° |
| revolutions per day: | 1.00274816 |
| mean anomaly at epoch: | 62.0893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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