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 26105.05722646 +.00000000 +00000-0 -13285-3 0 00007
2 00050 47.2340 357.6775 0113135 186.8521 173.0724 12.20163559 00
| Epoch (UTC): | 15 April 2026 01:22:24 |
| Eccentricity: | 0.0113135 |
| inclination: | 47.2340° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 357.6775° |
| argument of perigee: | 186.8521° |
| revolutions per day: | 12.20163559 |
| mean anomaly at epoch: | 173.0724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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