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 58242U 26145.17614581 +.00000000 +00000-0 +88345-5 0 00008
2 58242 43.0037 213.1362 0001988 275.4319 84.6306 15.27588011 00
| Epoch (UTC): | 25 May 2026 04:13:38 |
| Eccentricity: | 0.0001988 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 213.1362° |
| argument of perigee: | 275.4319° |
| revolutions per day: | 15.27588011 |
| mean anomaly at epoch: | 84.6306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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