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 57742U 26145.30560397 +.00000000 +00000-0 +45376-4 0 00008
2 57742 43.0022 99.7895 0001050 265.3334 94.7398 15.27574609 03
| Epoch (UTC): | 25 May 2026 07:20:04 |
| Eccentricity: | 0.0001050 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.7895° |
| argument of perigee: | 265.3334° |
| revolutions per day: | 15.27574609 |
| mean anomaly at epoch: | 94.7398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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