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 60589U 26145.48265490 +.00000000 +00000-0 +35468-4 0 00007
2 60589 53.1601 310.6932 0001016 84.5182 275.5935 15.30198777 00
| Epoch (UTC): | 25 May 2026 11:35:01 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1601° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6932° |
| argument of perigee: | 84.5182° |
| revolutions per day: | 15.30198777 |
| mean anomaly at epoch: | 275.5935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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