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 60314U 26145.44264088 +.00000000 +00000-0 -60583-4 0 00008
2 60314 53.1614 300.3979 0000846 69.7542 290.3549 15.30179861 01
| Epoch (UTC): | 25 May 2026 10:37:24 |
| Eccentricity: | 0.0000846 |
| inclination: | 53.1614° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.3979° |
| argument of perigee: | 69.7542° |
| revolutions per day: | 15.30179861 |
| mean anomaly at epoch: | 290.3549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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