View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 60620U 24140V 24357.87041252 .00001468 00000-0 33138-3 0 9995
2 60620 89.0360 335.3396 0112219 316.5830 42.6579 14.51987451 19936
| Epoch (UTC): | 22 December 2024 20:53:23 |
| Eccentricity: | 0.0112219 |
| inclination: | 89.0360° |
| perigee height: | 639 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 335.3396° |
| argument of perigee: | 316.5830° |
| revolutions per day: | 14.51987451 |
| mean anomaly at epoch: | 42.6579° |
| orbit number at epoch: | 1993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|