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 58208U 26145.36829554 +.00000000 +00000-0 +11871-5 0 00009
2 58208 43.0041 121.4110 0001430 281.7970 78.2722 15.27577241 08
| Epoch (UTC): | 25 May 2026 08:50:20 |
| Eccentricity: | 0.0001430 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.4110° |
| argument of perigee: | 281.7970° |
| revolutions per day: | 15.27577241 |
| mean anomaly at epoch: | 78.2722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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