View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00029U 60002B 24254.73822240 .00004288 00000-0 63187-3 0 9994
2 00029 48.3764 203.7202 0023026 14.3136 345.8424 14.76780988446802
| Epoch (UTC): | 10 September 2024 17:43:02 |
| Eccentricity: | 0.0023026 |
| inclination: | 48.3764° |
| perigee height: | 623 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 203.7202° |
| argument of perigee: | 14.3136° |
| revolutions per day: | 14.76780988 |
| mean anomaly at epoch: | 345.8424° |
| orbit number at epoch: | 44680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|