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 58741U 26145.30223183 +.00000000 +00000-0 -72093-5 0 00005
2 58741 43.0008 146.8334 0000897 267.8266 92.2483 15.27573458 07
| Epoch (UTC): | 25 May 2026 07:15:12 |
| Eccentricity: | 0.0000897 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.8334° |
| argument of perigee: | 267.8266° |
| revolutions per day: | 15.27573458 |
| mean anomaly at epoch: | 92.2483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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