View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25977U 99064A 24280.91575629 .00005388 00000-0 63812-3 0 9995
2 25977 98.2241 156.2395 0001049 32.9294 327.1985 14.85001956608190
| Epoch (UTC): | 06 October 2024 21:58:41 |
| Eccentricity: | 0.0001049 |
| inclination: | 98.2241° |
| perigee height: | 613 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 156.2395° |
| argument of perigee: | 32.9294° |
| revolutions per day: | 14.85001956 |
| mean anomaly at epoch: | 327.1985° |
| orbit number at epoch: | 60819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|