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 57415U 26145.53835330 +.00000000 +00000-0 +16243-3 0 00002
2 57415 43.0041 174.5181 0001726 282.3406 77.7252 15.27576340 04
| Epoch (UTC): | 25 May 2026 12:55:13 |
| Eccentricity: | 0.0001726 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.5181° |
| argument of perigee: | 282.3406° |
| revolutions per day: | 15.27576340 |
| mean anomaly at epoch: | 77.7252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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