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 59670U 26145.52116220 +.00000000 +00000-0 +70578-4 0 00008
2 59670 43.0004 324.4225 0001194 272.5486 87.5229 15.27581345 05
| Epoch (UTC): | 25 May 2026 12:30:28 |
| Eccentricity: | 0.0001194 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.4225° |
| argument of perigee: | 272.5486° |
| revolutions per day: | 15.27581345 |
| mean anomaly at epoch: | 87.5229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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