View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 60235U 24128A 25136.50282812 .00001975 00000-0 17609-3 0 9996
2 60235 61.9928 168.3541 0054107 44.0578 316.4803 14.98582771 46508
Epoch (UTC): | 16 May 2025 12:04:04 |
Eccentricity: | 0.0054107 |
inclination: | 61.9928° |
perigee height: | 533 km |
apogee height: | 609 km |
right ascension of ascending node: | 168.3541° |
argument of perigee: | 44.0578° |
revolutions per day: | 14.98582771 |
mean anomaly at epoch: | 316.4803° |
orbit number at epoch: | 4650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|