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 00050U 26104.15633310 +.00000000 +00000-0 -11733-4 0 00003
2 00050 47.2340 0.4737 0113118 184.1728 175.8125 12.20163559 07
| Epoch (UTC): | 14 April 2026 03:45:07 |
| Eccentricity: | 0.0113118 |
| inclination: | 47.2340° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 0.4737° |
| argument of perigee: | 184.1728° |
| revolutions per day: | 12.20163559 |
| mean anomaly at epoch: | 175.8125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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