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 58214U 26145.39384975 +.00000000 +00000-0 +53060-4 0 00007
2 58214 43.0034 120.7614 0001667 273.7420 86.3241 15.27581989 01
| Epoch (UTC): | 25 May 2026 09:27:08 |
| Eccentricity: | 0.0001667 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.7614° |
| argument of perigee: | 273.7420° |
| revolutions per day: | 15.27581989 |
| mean anomaly at epoch: | 86.3241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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