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 60458U 26145.67186824 +.00000000 +00000-0 +45682-3 0 00004
2 60458 35.0051 282.9519 0004841 11.3513 348.7314 15.35028991 09
| Epoch (UTC): | 25 May 2026 16:07:29 |
| Eccentricity: | 0.0004841 |
| inclination: | 35.0051° |
| perigee height: | 458 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 282.9519° |
| argument of perigee: | 11.3513° |
| revolutions per day: | 15.35028991 |
| mean anomaly at epoch: | 348.7314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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