View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27608U 02058D 24280.87425354 .00005423 00000-0 70151-3 0 9993
2 27608 64.5542 134.9380 0022987 9.8842 350.2711 14.81650000175083
| Epoch (UTC): | 06 October 2024 20:58:55 |
| Eccentricity: | 0.0022987 |
| inclination: | 64.5542° |
| perigee height: | 608 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 134.9380° |
| argument of perigee: | 9.8842° |
| revolutions per day: | 14.81650000 |
| mean anomaly at epoch: | 350.2711° |
| orbit number at epoch: | 17508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|