View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60312U 26145.24592044 +.00000000 +00000-0 +11738-4 0 00007
2 60312 53.1587 129.1510 0000937 78.9243 281.1881 15.69705115 03
| Epoch (UTC): | 25 May 2026 05:54:07 |
| Eccentricity: | 0.0000937 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 129.1510° |
| argument of perigee: | 78.9243° |
| revolutions per day: | 15.69705115 |
| mean anomaly at epoch: | 281.1881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|