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 57379U 26145.53594132 +.00000000 +00000-0 +26164-4 0 00007
2 57379 43.0023 164.1312 0001185 277.0438 83.0279 15.27578037 03
| Epoch (UTC): | 25 May 2026 12:51:45 |
| Eccentricity: | 0.0001185 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.1312° |
| argument of perigee: | 277.0438° |
| revolutions per day: | 15.27578037 |
| mean anomaly at epoch: | 83.0279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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