View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24726U 97006B 23083.92129500 .00000026 00000-0 84895-4 0 9993
2 24726 82.5962 293.2479 0004262 239.7635 120.3034 12.61353855201678
| Epoch (UTC): | 24 March 2023 22:06:39 |
| Eccentricity: | 0.0004262 |
| inclination: | 82.5962° |
| perigee height: | 1414 km |
| apogee height: | 1420 km |
| right ascension of ascending node: | 293.2479° |
| argument of perigee: | 239.7635° |
| revolutions per day: | 12.61353855 |
| mean anomaly at epoch: | 120.3034° |
| orbit number at epoch: | 20167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|