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 58193U 26145.07207552 +.00000000 +00000-0 +10894-3 0 00000
2 58193 43.0070 72.2999 0003051 293.1946 66.8584 15.27595617 08
| Epoch (UTC): | 25 May 2026 01:43:47 |
| Eccentricity: | 0.0003051 |
| inclination: | 43.0070° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 72.2999° |
| argument of perigee: | 293.1946° |
| revolutions per day: | 15.27595617 |
| mean anomaly at epoch: | 66.8584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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