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 26045.76120977 +.00000000 +00000-0 +27269-3 0 00003
2 00050 47.2291 181.7306 0113078 10.1301 350.1733 12.20162703 00
| Epoch (UTC): | 14 February 2026 18:16:08 |
| Eccentricity: | 0.0113078 |
| inclination: | 47.2291° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 181.7306° |
| argument of perigee: | 10.1301° |
| revolutions per day: | 12.20162703 |
| mean anomaly at epoch: | 350.1733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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