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 50322U 26144.67083537 +.00000000 +00000-0 +00000-0 0 00001
2 50322 3.6161 80.2270 0002247 47.7666 66.0515 1.00492065 01
| Epoch (UTC): | 24 May 2026 16:06:00 |
| Eccentricity: | 0.0002247 |
| inclination: | 3.6161° |
| perigee height: | 35716 km |
| apogee height: | 35734 km |
| right ascension of ascending node: | 80.2270° |
| argument of perigee: | 47.7666° |
| revolutions per day: | 1.00492065 |
| mean anomaly at epoch: | 66.0515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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