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 58064U 26145.19548762 +.00000000 +00000-0 +26672-4 0 00003
2 58064 43.0043 314.7247 0001674 281.1195 78.9469 15.27586641 00
| Epoch (UTC): | 25 May 2026 04:41:30 |
| Eccentricity: | 0.0001674 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 314.7247° |
| argument of perigee: | 281.1195° |
| revolutions per day: | 15.27586641 |
| mean anomaly at epoch: | 78.9469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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