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 58222U 26145.30676301 +.00000000 +00000-0 -11169-4 0 00009
2 58222 43.0027 121.8015 0001543 268.3927 91.6748 15.27576747 01
| Epoch (UTC): | 25 May 2026 07:21:44 |
| Eccentricity: | 0.0001543 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.8015° |
| argument of perigee: | 268.3927° |
| revolutions per day: | 15.27576747 |
| mean anomaly at epoch: | 91.6748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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