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 60050U 26145.27522294 +.00000000 +00000-0 +13487-4 0 00002
2 60050 53.1603 248.4354 0000751 55.6716 304.4373 15.69710753 02
| Epoch (UTC): | 25 May 2026 06:36:19 |
| Eccentricity: | 0.0000751 |
| inclination: | 53.1603° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 248.4354° |
| argument of perigee: | 55.6716° |
| revolutions per day: | 15.69710753 |
| mean anomaly at epoch: | 304.4373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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