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 57741U 26145.21965381 +.00000000 +00000-0 +40477-4 0 00006
2 57741 43.0019 100.0040 0001234 268.5699 91.5011 15.27581497 09
| Epoch (UTC): | 25 May 2026 05:16:18 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.0040° |
| argument of perigee: | 268.5699° |
| revolutions per day: | 15.27581497 |
| mean anomaly at epoch: | 91.5011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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