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 58402U 26145.23979388 +.00000000 +00000-0 +54736-4 0 00008
2 58402 43.0059 340.2065 0001414 276.5418 83.5273 15.27582240 09
| Epoch (UTC): | 25 May 2026 05:45:18 |
| Eccentricity: | 0.0001414 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 340.2065° |
| argument of perigee: | 276.5418° |
| revolutions per day: | 15.27582240 |
| mean anomaly at epoch: | 83.5273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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