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 57740U 26145.38126701 +.00000000 +00000-0 +39175-4 0 00001
2 57740 43.0053 26.2886 0001081 282.0199 78.0531 15.27588435 05
| Epoch (UTC): | 25 May 2026 09:09:01 |
| Eccentricity: | 0.0001081 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 26.2886° |
| argument of perigee: | 282.0199° |
| revolutions per day: | 15.27588435 |
| mean anomaly at epoch: | 78.0531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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