View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27006U 01056F 24281.87375826 .00000091 00000-0 15324-3 0 9998
2 27006 99.7037 69.9953 0013926 236.3517 247.9644 13.71045997142235
| Epoch (UTC): | 07 October 2024 20:58:12 |
| Eccentricity: | 0.0013926 |
| inclination: | 99.7037° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 69.9953° |
| argument of perigee: | 236.3517° |
| revolutions per day: | 13.71045997 |
| mean anomaly at epoch: | 247.9644° |
| orbit number at epoch: | 14223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|