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 57434U 26145.59988514 +.00000000 +00000-0 -29943-4 0 00005
2 57434 42.9999 185.5546 0001300 269.3405 90.7298 15.27575647 08
| Epoch (UTC): | 25 May 2026 14:23:50 |
| Eccentricity: | 0.0001300 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.5546° |
| argument of perigee: | 269.3405° |
| revolutions per day: | 15.27575647 |
| mean anomaly at epoch: | 90.7298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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