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 57129U 26145.55717333 +.00000000 +00000-0 +17474-4 0 00006
2 57129 43.0002 189.7204 0001220 270.3948 89.6764 15.27576305 05
| Epoch (UTC): | 25 May 2026 13:22:19 |
| Eccentricity: | 0.0001220 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.7204° |
| argument of perigee: | 270.3948° |
| revolutions per day: | 15.27576305 |
| mean anomaly at epoch: | 89.6764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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