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 00446U 26104.11767814 +.00000000 +00000-0 +21200-4 0 00004
2 00446 50.1415 226.7589 0070267 185.2051 347.4904 13.35361698 01
| Epoch (UTC): | 14 April 2026 02:49:27 |
| Eccentricity: | 0.0070267 |
| inclination: | 50.1415° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 226.7589° |
| argument of perigee: | 185.2051° |
| revolutions per day: | 13.35361698 |
| mean anomaly at epoch: | 347.4904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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