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 58227U 26145.62213235 +.00000000 +00000-0 -10861-4 0 00000
2 58227 43.0021 119.8807 0000892 262.7829 97.2921 15.27585570 00
| Epoch (UTC): | 25 May 2026 14:55:52 |
| Eccentricity: | 0.0000892 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 119.8807° |
| argument of perigee: | 262.7829° |
| revolutions per day: | 15.27585570 |
| mean anomaly at epoch: | 97.2921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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