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 57372U 26145.43936802 +.00000000 +00000-0 +27719-4 0 00000
2 57372 43.0007 168.5232 0001001 289.0462 71.0281 15.27576007 09
| Epoch (UTC): | 25 May 2026 10:32:41 |
| Eccentricity: | 0.0001001 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.5232° |
| argument of perigee: | 289.0462° |
| revolutions per day: | 15.27576007 |
| mean anomaly at epoch: | 71.0281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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