View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27422U 02021B 22228.43561322 .00000132 00000-0 68211-4 0 9992
2 27422 98.4516 172.6412 0013342 62.1339 298.1193 14.29437244 58020
| Epoch (UTC): | 16 August 2022 10:27:16 |
| Eccentricity: | 0.0013342 |
| inclination: | 98.4516° |
| perigee height: | 784 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 172.6412° |
| argument of perigee: | 62.1339° |
| revolutions per day: | 14.29437244 |
| mean anomaly at epoch: | 298.1193° |
| orbit number at epoch: | 5802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|