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 57789U 26144.89950110 +.00000000 +00000-0 +67800-4 0 00004
2 57789 43.0002 7.9822 0001305 270.0885 89.9818 15.27581898 01
| Epoch (UTC): | 24 May 2026 21:35:16 |
| Eccentricity: | 0.0001305 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.9822° |
| argument of perigee: | 270.0885° |
| revolutions per day: | 15.27581898 |
| mean anomaly at epoch: | 89.9818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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