View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00446U 26106.55446124 +.00000000 +00000-0 +37206-4 0 00005
2 00446 50.1414 217.9510 0070270 192.4566 181.8217 13.35361818 02
| Epoch (UTC): | 16 April 2026 13:18:25 |
| Eccentricity: | 0.0070270 |
| inclination: | 50.1414° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 217.9510° |
| argument of perigee: | 192.4566° |
| revolutions per day: | 13.35361818 |
| mean anomaly at epoch: | 181.8217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|