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 58240U 26145.18128021 +.00000000 +00000-0 +29940-4 0 00001
2 58240 43.0032 213.1721 0001693 267.5542 92.5116 15.27577869 01
| Epoch (UTC): | 25 May 2026 04:21:02 |
| Eccentricity: | 0.0001693 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 213.1721° |
| argument of perigee: | 267.5542° |
| revolutions per day: | 15.27577869 |
| mean anomaly at epoch: | 92.5116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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