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 26044.77838655 +.00000000 +00000-0 +28575-3 0 00003
2 00050 47.2290 184.7812 0113100 7.1979 353.0405 12.20162676 04
| Epoch (UTC): | 13 February 2026 18:40:52 |
| Eccentricity: | 0.0113100 |
| inclination: | 47.2290° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 184.7812° |
| argument of perigee: | 7.1979° |
| revolutions per day: | 12.20162676 |
| mean anomaly at epoch: | 353.0405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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