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 58221U 26145.42211987 +.00000000 +00000-0 +13466-3 0 00006
2 58221 42.9990 120.9690 0001246 268.2462 91.8247 15.27595508 01
| Epoch (UTC): | 25 May 2026 10:07:51 |
| Eccentricity: | 0.0001246 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.9690° |
| argument of perigee: | 268.2462° |
| revolutions per day: | 15.27595508 |
| mean anomaly at epoch: | 91.8247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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