View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61061U 26145.38915417 +.00000000 +00000-0 +23035-4 0 00000
2 61061 53.1581 293.2939 0000878 79.3562 280.7555 15.69713944 02
| Epoch (UTC): | 25 May 2026 09:20:22 |
| Eccentricity: | 0.0000878 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 293.2939° |
| argument of perigee: | 79.3562° |
| revolutions per day: | 15.69713944 |
| mean anomaly at epoch: | 280.7555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|