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 58213U 26145.40542034 +.00000000 +00000-0 +14387-3 0 00008
2 58213 43.0023 120.8469 0001401 288.5559 71.5140 15.27565952 06
| Epoch (UTC): | 25 May 2026 09:43:48 |
| Eccentricity: | 0.0001401 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.8469° |
| argument of perigee: | 288.5559° |
| revolutions per day: | 15.27565952 |
| mean anomaly at epoch: | 71.5140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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