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 58435U 26145.52885589 +.00000000 +00000-0 +12297-3 0 00000
2 58435 96.6814 249.9645 0008331 197.9507 162.1475 15.90081652 06
| Epoch (UTC): | 25 May 2026 12:41:33 |
| Eccentricity: | 0.0008331 |
| inclination: | 96.6814° |
| perigee height: | 296 km |
| apogee height: | 308 km |
| right ascension of ascending node: | 249.9645° |
| argument of perigee: | 197.9507° |
| revolutions per day: | 15.90081652 |
| mean anomaly at epoch: | 162.1475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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