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 58068U 26145.47839593 +.00000000 +00000-0 -30809-4 0 00001
2 58068 43.0030 316.8037 0001434 251.1030 108.9666 15.27554221 01
| Epoch (UTC): | 25 May 2026 11:28:53 |
| Eccentricity: | 0.0001434 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.8037° |
| argument of perigee: | 251.1030° |
| revolutions per day: | 15.27554221 |
| mean anomaly at epoch: | 108.9666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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