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 58340U 26145.22257391 +.00000000 +00000-0 +41586-3 0 00009
2 58340 97.3967 234.8462 0006404 186.6919 173.4244 15.43908949 03
| Epoch (UTC): | 25 May 2026 05:20:30 |
| Eccentricity: | 0.0006404 |
| inclination: | 97.3967° |
| perigee height: | 430 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 234.8462° |
| argument of perigee: | 186.6919° |
| revolutions per day: | 15.43908949 |
| mean anomaly at epoch: | 173.4244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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