View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00053U 60009E 23084.27346311 -.00000074 00000-0 10046-3 0 9993
2 00053 47.2796 21.6842 0097759 188.8643 171.0420 12.17292883791693
| Epoch (UTC): | 25 March 2023 06:33:47 |
| Eccentricity: | 0.0097759 |
| inclination: | 47.2796° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 21.6842° |
| argument of perigee: | 188.8643° |
| revolutions per day: | 12.17292883 |
| mean anomaly at epoch: | 171.0420° |
| orbit number at epoch: | 79169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|