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 60196U 26145.46072197 +.00000000 +00000-0 +16376-4 0 00006
2 60196 53.1611 325.6237 0001359 108.8656 251.2493 15.31705970 05
| Epoch (UTC): | 25 May 2026 11:03:26 |
| Eccentricity: | 0.0001359 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 325.6237° |
| argument of perigee: | 108.8656° |
| revolutions per day: | 15.31705970 |
| mean anomaly at epoch: | 251.2493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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