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 58219U 26145.61185289 +.00000000 +00000-0 +58542-3 0 00003
2 58219 42.9991 119.8122 0001295 274.3520 85.7183 15.27593768 00
| Epoch (UTC): | 25 May 2026 14:41:04 |
| Eccentricity: | 0.0001295 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 119.8122° |
| argument of perigee: | 274.3520° |
| revolutions per day: | 15.27593768 |
| mean anomaly at epoch: | 85.7183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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