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 23336.00595201 .00003290 00000-0 56865-3 0 9995
2 27939 98.2647 124.5416 0011683 331.3575 140.5105 14.69045499 79178
| Epoch (UTC): | 02 December 2023 00:08:34 |
| Eccentricity: | 0.0011683 |
| inclination: | 98.2647° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 124.5416° |
| argument of perigee: | 331.3575° |
| revolutions per day: | 14.69045499 |
| mean anomaly at epoch: | 140.5105° |
| orbit number at epoch: | 7917 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|