View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05043U 71019 A 71130.00000000 .00000000 +00000-0 +00000-0 0 9992
2 05043 031.3520 224.6786 9195299 311.8548 290.0032 00.24135506000122
| Epoch (UTC): | 10 May 1971 00:00:00 |
| Eccentricity: | 0.9195299 |
| inclination: | 31.3520° |
| perigee height: | 2390 km |
| apogee height: | 202786 km |
| right ascension of ascending node: | 224.6786° |
| argument of perigee: | 311.8548° |
| revolutions per day: | 0.24135506 |
| mean anomaly at epoch: | 290.0032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|