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 54846U 26145.45420955 +.00000000 +00000-0 +59846-5 0 00009
2 54846 43.0036 59.1060 0000839 236.3077 123.7694 15.27580146 05
| Epoch (UTC): | 25 May 2026 10:54:03 |
| Eccentricity: | 0.0000839 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 59.1060° |
| argument of perigee: | 236.3077° |
| revolutions per day: | 15.27580146 |
| mean anomaly at epoch: | 123.7694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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