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 57899U 26145.31356934 +.00000000 +00000-0 +45486-4 0 00004
2 57899 43.0062 241.5826 0001734 265.4488 94.6165 15.27578560 02
| Epoch (UTC): | 25 May 2026 07:31:32 |
| Eccentricity: | 0.0001734 |
| inclination: | 43.0062° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 241.5826° |
| argument of perigee: | 265.4488° |
| revolutions per day: | 15.27578560 |
| mean anomaly at epoch: | 94.6165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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