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 26112.30990655 +.00000000 +00000-0 +14193-3 0 00004
2 50466 98.4948 205.0116 0002877 262.9006 97.1856 14.41301714 01
| Epoch (UTC): | 22 April 2026 07:26:15 |
| Eccentricity: | 0.0002877 |
| inclination: | 98.4948° |
| perigee height: | 752 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 205.0116° |
| argument of perigee: | 262.9006° |
| revolutions per day: | 14.41301714 |
| mean anomaly at epoch: | 97.1856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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