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 57771U 26145.38372462 +.00000000 +00000-0 +28535-4 0 00000
2 57771 43.0016 121.5851 0001244 306.1218 53.9519 15.27578151 02
| Epoch (UTC): | 25 May 2026 09:12:33 |
| Eccentricity: | 0.0001244 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.5851° |
| argument of perigee: | 306.1218° |
| revolutions per day: | 15.27578151 |
| mean anomaly at epoch: | 53.9519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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