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 64058U 26145.63371639 +.00000000 +00000-0 +36796-4 0 00007
2 64058 44.9824 122.7144 0012664 274.7397 85.1989 13.99144652 09
| Epoch (UTC): | 25 May 2026 15:12:33 |
| Eccentricity: | 0.0012664 |
| inclination: | 44.9824° |
| perigee height: | 888 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 122.7144° |
| argument of perigee: | 274.7397° |
| revolutions per day: | 13.99144652 |
| mean anomaly at epoch: | 85.1989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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