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 58742U 26145.44071529 +.00000000 +00000-0 +22131-4 0 00002
2 58742 43.0034 146.1510 0000994 263.7378 96.3360 15.27574641 07
| Epoch (UTC): | 25 May 2026 10:34:37 |
| Eccentricity: | 0.0000994 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.1510° |
| argument of perigee: | 263.7378° |
| revolutions per day: | 15.27574641 |
| mean anomaly at epoch: | 96.3360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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