View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20929U 90095A 19035.35742763 0.00000000 00000-0 00000-0 0 03
2 20929 15.3988 5.2758 0007338 7.4830 352.5399 0.98394720 06
| Epoch (UTC): | 04 February 2019 08:34:41 |
| Eccentricity: | 0.0007338 |
| inclination: | 15.3988° |
| perigee height: | 36289 km |
| apogee height: | 36352 km |
| right ascension of ascending node: | 5.2758° |
| argument of perigee: | 7.4830° |
| revolutions per day: | 0.98394720 |
| mean anomaly at epoch: | 352.5399° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|