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 58234U 26145.21968866 +.00000000 +00000-0 -44246-5 0 00005
2 58234 43.0007 212.6227 0001090 277.7184 82.3544 15.27578297 05
| Epoch (UTC): | 25 May 2026 05:16:21 |
| Eccentricity: | 0.0001090 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.6227° |
| argument of perigee: | 277.7184° |
| revolutions per day: | 15.27578297 |
| mean anomaly at epoch: | 82.3544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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