View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27939U 03042A 22141.93961579 .00001378 00000-0 25270-3 0 9996
2 27939 98.1884 282.6730 0011575 293.0238 66.9748 14.67321402997155
| Epoch (UTC): | 21 May 2022 22:33:02 |
| Eccentricity: | 0.0011575 |
| inclination: | 98.1884° |
| perigee height: | 661 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 282.6730° |
| argument of perigee: | 293.0238° |
| revolutions per day: | 14.67321402 |
| mean anomaly at epoch: | 66.9748° |
| orbit number at epoch: | 99715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|