View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29260U 06030A 19326.84410686 .99999999 30221-5 10877-2 0 9996
2 29260 63.1487 67.7227 0589461 248.2138 249.1435 15.29862549 98110
| Epoch (UTC): | 22 November 2019 20:15:30 |
| Eccentricity: | 0.0589461 |
| inclination: | 63.1487° |
| perigee height: | 72 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 67.7227° |
| argument of perigee: | 248.2138° |
| revolutions per day: | 15.29862549 |
| mean anomaly at epoch: | 249.1435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|