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 57352U 26145.48805807 +.00000000 +00000-0 +19006-4 0 00003
2 57352 43.0002 168.0505 0001282 270.4723 89.5982 15.27584520 06
| Epoch (UTC): | 25 May 2026 11:42:48 |
| Eccentricity: | 0.0001282 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.0505° |
| argument of perigee: | 270.4723° |
| revolutions per day: | 15.27584520 |
| mean anomaly at epoch: | 89.5982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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