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 26037.40721146 +.00000000 +00000-0 -17123-3 0 00009
2 00050 47.2283 207.6618 0113229 345.2567 14.4933 12.20162737 08
| Epoch (UTC): | 06 February 2026 09:46:23 |
| Eccentricity: | 0.0113229 |
| inclination: | 47.2283° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 207.6618° |
| argument of perigee: | 345.2567° |
| revolutions per day: | 12.20162737 |
| mean anomaly at epoch: | 14.4933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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