View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00050U 60009B 23338.47081232 -.00000019 00000-0 62796-3 0 9990
2 00050 47.2277 155.0350 0113771 135.7219 225.2739 12.20135996824678
| Epoch (UTC): | 04 December 2023 11:17:58 |
| Eccentricity: | 0.0113771 |
| inclination: | 47.2277° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 155.0350° |
| argument of perigee: | 135.7219° |
| revolutions per day: | 12.20135996 |
| mean anomaly at epoch: | 225.2739° |
| orbit number at epoch: | 82467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|