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 58217U 26145.40411448 +.00000000 +00000-0 +25703-3 0 00000
2 58217 43.0044 120.8353 0002107 260.2509 99.8105 15.27607005 01
| Epoch (UTC): | 25 May 2026 09:41:55 |
| Eccentricity: | 0.0002107 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.8353° |
| argument of perigee: | 260.2509° |
| revolutions per day: | 15.27607005 |
| mean anomaly at epoch: | 99.8105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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