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 58057U 26145.19932770 +.00000000 +00000-0 +10164-3 0 00009
2 58057 43.0035 314.7526 0001457 268.7202 91.3482 15.27586974 05
| Epoch (UTC): | 25 May 2026 04:47:01 |
| Eccentricity: | 0.0001457 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 314.7526° |
| argument of perigee: | 268.7202° |
| revolutions per day: | 15.27586974 |
| mean anomaly at epoch: | 91.3482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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