View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60061U 26145.36465623 +.00000000 +00000-0 -90518-6 0 00009
2 60061 53.1584 173.2469 0000769 13.0139 347.0899 15.69689569 06
| Epoch (UTC): | 25 May 2026 08:45:06 |
| Eccentricity: | 0.0000769 |
| inclination: | 53.1584° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 173.2469° |
| argument of perigee: | 13.0139° |
| revolutions per day: | 15.69689569 |
| mean anomaly at epoch: | 347.0899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|