View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22286U 92094A 23150.94709526 .00001729 00000-0 17575-3 0 9994
2 22286 82.5181 122.3010 0022354 98.2253 262.1502 14.90056049624740
| Epoch (UTC): | 30 May 2023 22:43:49 |
| Eccentricity: | 0.0022354 |
| inclination: | 82.5181° |
| perigee height: | 582 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 122.3010° |
| argument of perigee: | 98.2253° |
| revolutions per day: | 14.90056049 |
| mean anomaly at epoch: | 262.1502° |
| orbit number at epoch: | 62474 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|