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 50816U 26145.52712255 +.00000000 +00000-0 +73669-3 0 00004
2 50816 53.2123 179.2867 0003037 42.2456 317.8773 15.16480792 03
| Epoch (UTC): | 25 May 2026 12:39:03 |
| Eccentricity: | 0.0003037 |
| inclination: | 53.2123° |
| perigee height: | 514 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 179.2867° |
| argument of perigee: | 42.2456° |
| revolutions per day: | 15.16480792 |
| mean anomaly at epoch: | 317.8773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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