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 60446U 26145.56295400 +.00000000 +00000-0 +90425-5 0 00007
2 60446 53.1594 209.6343 0000894 77.9030 282.2071 15.30191463 08
| Epoch (UTC): | 25 May 2026 13:30:39 |
| Eccentricity: | 0.0000894 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.6343° |
| argument of perigee: | 77.9030° |
| revolutions per day: | 15.30191463 |
| mean anomaly at epoch: | 282.2071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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