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 57351U 26145.47554782 +.00000000 +00000-0 +16789-4 0 00009
2 57351 43.0036 175.0159 0001796 286.1393 73.9261 15.27575548 09
| Epoch (UTC): | 25 May 2026 11:24:47 |
| Eccentricity: | 0.0001796 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.0159° |
| argument of perigee: | 286.1393° |
| revolutions per day: | 15.27575548 |
| mean anomaly at epoch: | 73.9261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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