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 58230U 26145.46300791 +.00000000 +00000-0 +18739-2 0 00009
2 58230 42.9916 212.6925 0005504 4.9316 355.1589 15.28312794 03
| Epoch (UTC): | 25 May 2026 11:06:43 |
| Eccentricity: | 0.0005504 |
| inclination: | 42.9916° |
| perigee height: | 477 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 212.6925° |
| argument of perigee: | 4.9316° |
| revolutions per day: | 15.28312794 |
| mean anomaly at epoch: | 355.1589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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