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 57743U 26145.55301679 +.00000000 +00000-0 +88124-4 0 00000
2 57743 42.9994 98.2050 0000924 285.8950 74.1800 15.27596922 09
| Epoch (UTC): | 25 May 2026 13:16:20 |
| Eccentricity: | 0.0000924 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.2050° |
| argument of perigee: | 285.8950° |
| revolutions per day: | 15.27596922 |
| mean anomaly at epoch: | 74.1800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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