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 58934U 26145.18820007 +.00000000 +00000-0 +45912-4 0 00001
2 58934 53.1604 314.0782 0001150 103.8916 256.2213 15.30189791 05
| Epoch (UTC): | 25 May 2026 04:31:00 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.0782° |
| argument of perigee: | 103.8916° |
| revolutions per day: | 15.30189791 |
| mean anomaly at epoch: | 256.2213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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