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 57073U 26145.02668122 +.00000000 +00000-0 +11855-4 0 00004
2 57073 43.0038 25.1415 0001031 247.8575 112.2168 15.27574374 09
| Epoch (UTC): | 25 May 2026 00:38:25 |
| Eccentricity: | 0.0001031 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.1415° |
| argument of perigee: | 247.8575° |
| revolutions per day: | 15.27574374 |
| mean anomaly at epoch: | 112.2168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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