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 26152.16239941 +.00000000 +00000-0 +38930-4 0 00005
2 00446 50.1429 53.0984 0070219 328.0446 192.8021 13.35362952 04
| Epoch (UTC): | 01 June 2026 03:53:51 |
| Eccentricity: | 0.0070219 |
| inclination: | 50.1429° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 53.0984° |
| argument of perigee: | 328.0446° |
| revolutions per day: | 13.35362952 |
| mean anomaly at epoch: | 192.8021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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