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 50466U 26145.63203166 +.00000000 +00000-0 +26115-3 0 00007
2 50466 98.4963 238.1455 0004618 151.0505 209.0941 14.41333551 01
| Epoch (UTC): | 25 May 2026 15:10:07 |
| Eccentricity: | 0.0004618 |
| inclination: | 98.4963° |
| perigee height: | 751 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 238.1455° |
| argument of perigee: | 151.0505° |
| revolutions per day: | 14.41333551 |
| mean anomaly at epoch: | 209.0941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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