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 57734U 26145.24663160 +.00000000 +00000-0 +40062-4 0 00001
2 57734 43.0033 100.1730 0000788 277.6775 82.3987 15.27580128 03
| Epoch (UTC): | 25 May 2026 05:55:08 |
| Eccentricity: | 0.0000788 |
| inclination: | 43.0033° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.1730° |
| argument of perigee: | 277.6775° |
| revolutions per day: | 15.27580128 |
| mean anomaly at epoch: | 82.3987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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