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 57816U 26145.50687478 +.00000000 +00000-0 +15028-3 0 00002
2 57816 43.0021 160.6095 0001864 276.1840 83.8799 15.27608403 03
| Epoch (UTC): | 25 May 2026 12:09:53 |
| Eccentricity: | 0.0001864 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.6095° |
| argument of perigee: | 276.1840° |
| revolutions per day: | 15.27608403 |
| mean anomaly at epoch: | 83.8799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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