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 26087.84469243 +.00000000 +00000-0 +49149-4 0 00001
2 00446 50.1412 285.5807 0070293 136.8732 238.4067 13.35360755 03
| Epoch (UTC): | 28 March 2026 20:16:21 |
| Eccentricity: | 0.0070293 |
| inclination: | 50.1412° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 285.5807° |
| argument of perigee: | 136.8732° |
| revolutions per day: | 13.35360755 |
| mean anomaly at epoch: | 238.4067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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