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 58246U 26145.50564757 +.00000000 +00000-0 +13006-4 0 00009
2 58246 43.0043 211.3219 0002146 295.9399 64.1231 15.27574975 08
| Epoch (UTC): | 25 May 2026 12:08:07 |
| Eccentricity: | 0.0002146 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 211.3219° |
| argument of perigee: | 295.9399° |
| revolutions per day: | 15.27574975 |
| mean anomaly at epoch: | 64.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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