View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00012U 59001B 23080.38516128 .00003127 00000-0 18515-2 0 9990
2 00012 32.9049 66.6708 1660639 331.8412 20.1306 11.45242631395365
Epoch (UTC): | 21 March 2023 09:14:37 |
Eccentricity: | 0.1660639 |
inclination: | 32.9049° |
perigee height: | 555 km |
apogee height: | 3316 km |
right ascension of ascending node: | 66.6708° |
argument of perigee: | 331.8412° |
revolutions per day: | 11.45242631 |
mean anomaly at epoch: | 20.1306° |
orbit number at epoch: | 39536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|