View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07970U 75057A 86174.55658840 .00284751 -16730-5 +20081-3 0 9998
2 07970 032.9313 249.7962 0002282 091.2540 268.8434 16.15015580616886
| Epoch (UTC): | 23 June 1986 13:21:29 |
| Eccentricity: | 0.0002282 |
| inclination: | 32.9313° |
| perigee height: | 231 km |
| apogee height: | 234 km |
| right ascension of ascending node: | 249.7962° |
| argument of perigee: | 91.2540° |
| revolutions per day: | 16.15015580 |
| mean anomaly at epoch: | 268.8434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|