View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 21949U 92023A 18121.82291481 0.00000000 00000-0 00000-0 0 02
2 21949 85.0087 344.9565 0003500 148.4393 211.5605 14.31404896 01
| Epoch (UTC): | 01 May 2018 19:44:59 |
| Eccentricity: | 0.0003500 |
| inclination: | 85.0087° |
| perigee height: | 784 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 344.9565° |
| argument of perigee: | 148.4393° |
| revolutions per day: | 14.31404896 |
| mean anomaly at epoch: | 211.5605° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|