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 57361U 26145.44194005 +.00000000 +00000-0 +11157-4 0 00009
2 57361 43.0016 168.5554 0001071 294.7000 65.3740 15.27576075 03
| Epoch (UTC): | 25 May 2026 10:36:23 |
| Eccentricity: | 0.0001071 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.5554° |
| argument of perigee: | 294.7000° |
| revolutions per day: | 15.27576075 |
| mean anomaly at epoch: | 65.3740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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